^;
TEXT-BOOK OF PHYSICS
PROPERTIES OF MATTER
A TEXT=BOOK OF PHYSICS
BY
Prof. J. H. POYNTING, Sir J. J. THOMSON,
SC.l)., I-.R.S., AND M.A., K.K.S.,
I.ate Fellow uf Trinity CoIIcrc, Cambridge ; Fellow of Trinity College, Cambridge ; Prof.
Professor of Physics, liirminghain of Experimental Physics m the University
University. of Cambridge.
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TEXT-BOOK OF PHYSICS
BY
J. H. POYNTING, Sc.D., F.R.S.
HON. Sc.D. VICTOKIA UNIVERSITY
LATE FELLOW OF TRINITY COLLEGE, CAMBRIDGE; MASON PROFESSOR
OF PnYSICS IN THE UNIVERSITY OF BIRMINGHAM
AND
Sir J. J. THOMSON, M.A., F.RS., Hon. Sc.D. Dublin
HON. D.L. PRINCETON; HON. Sc.D. VICTORIA: HON. LL.D. GLASGOW
HON. Pn.D. CRACOW
FELLOW OF TRINITY COLLEGE, CAMBRIDGE ; CAVENDISH PROFESSOR OF
EXPERIMENTAL PHYSICS IN THE UNIVERSITY OF CAMBRIDGE;
PROFESSOR OF NATURAL PHILOSOPHY AT THE
ROYAL INSTITDTION
PROPERTIES OF MATTER
WITH i58 ILLUSTRATIONS
FIFTH EDITION, CAREFULLY PiE VISED
LONDON
CHARLES GRIFFIN AND COMPANY, LIMITED
EXETER STREET, STRAND
1909
\_AU r'ights reserred]
6?
c
nh
PREFACE.
The volume now presented must be regardecl as tlie opening
one of a series forming a Text-Book on Physics, which the
authors are preparing. The second volume, that on Sound, has
already been issued, and the remaining volumes dealing with
Heat, Magnetism and Electricity, and Light will be published
in succession. ..-
As already-stated in the preface to the volume on Sound,
" The Text-Book is intended chiefly for the use of students who
lay most stress on the study of the experimental part of
Physics, and who have not yet reached the stage at which the
reading of advanced treatises on special subjects is desirable.
To bring the subject within the compass thus prescribed, an
account is given only of phenomena which are of special
importance, or which appear to throw light on other branches
of Physics, and the mathematical methods adopted are very
elementary. The student who possesses a knowledge of
advanced mathematical methods, and who knows how to use
them, will, no doubt, be able to work out and remember most
easily a theory which uses such methods. But at present a
large number of earnest students of Physics are not so
equipped, and the authors aim at giving an account of the
subject which will be useful to students of this class. Even
for the reader who is mathematically trained, there is some
advantage in the study of elementary methods, compensating
for their cumbrous form. They bring before us more evidently
vi PREFACE
the points at wliich the various assumptions are made, and they
render more prominent the conditions under which the theory-
holds good."
In the present volume the authors deal with weight, mass,
gravitation, and those properties of matter which relate chiefly
to change of form, such as Elasticity, Fluid Viscosity, Surface
Tension, Diffusion and Solution. The molecular theory of matter
has necessarily been introduced, inasmuch as investigators have
almost always expressed their work in terms of that theory.
But the detailed account of the theory, especially as applied to
gases, will be given in the volume on Heat, in connection with
the account of the phenomena which first brought it into
prominence.
PEEFACE TO FIFTH EDITION.
A FEW corrections have been made in this edition. The authors
desire to thank the readers who have kindly pointed out errors
and have enabled them to make these corrections.
J. H. P.
J. J. T.
Jamiary 1909.
CONTENTS
CHAP.
I. VVEIGIIT AND MASS .......
II. THE ACCELERATION OF GRAVITY. ITS VARIATION AND
THE FIGURE OF THE EARTH ....
III. GRAVITATION
IV. ELASTICITY
V. STRAIN
VI. STRESSES. RELATION BETWEEN STRESSES AND STRAINS
VII. TORSION
VIII. BENDING OF RODS
IX. SPIRAL SPRINGS
X. IMPACT
XI. COMPRESSIBILITY OF LIQUIDS ....
XII. THE RELATION BETWEEN THE PRESSURE AND VOLUME 01
A GAS
XIII. REVERSIBLE THERMAL EFFECTS ACCOMPANYING ALTERA
TIONS IN STRAINS
XIV. CAPILLARITY
XV. LAPLACE'S THEORY OF CAPILLARITY
XVI. DIFFUSION OF LIQUIDS
XVII. DIFFUSION OF GASES
XVIII. VISCOSITY OF LIQUIDS .....
INDEX ........
PAGE
7
28
53
62
68
85
103
109
116
124
131
135
173
182
196
205
225
PROPERTIES OF MATTER.
CHAPTEK I.
WEIGHT AND MASS.
Contents.— Weiglit — Mass — Definition of Mass— Mass proportional to Weight at
the same Point — Constancy of Mass — Unit of Mass.
Introductory Remarks. — Physics is the study of the properties of
matter, and of the action of one portion of matter upon another, and
ultimately of the effects of these actions upon our senses. The properties
studied in the various branches, Sound, Heat, Light, and Magnetism and
Electricity, are for the most part easily classified under these headings.
But there are other properties chiefly connected with changes in shape and
relative position within a system which are grouped together as " General
Properties of INIatter." Among these latter properties are Elasticity,
Surface Tension, Diffusion and Viscosity.
The most general properties of matter are really those studied in
Statics and Dynamics : the relation between forces, when the matter
acted on is in equilibrium and the motion of matter under the mutual
action of the various portions of a system. But in Statics and Dynamics
the recourse to experiment is so small, and when the experimental foun-
dation is once laid the mathematical structure is so great, that it is con-
venient to treat these branches of Physics separately. We shall assume
in this work that the reader has already studied them, and is familiar
both with the conditions of equilibrium and with the simpler types of
motion.
We shall, however, begin with the discussion of some questions which
involve dynamical considerations. We shall show how we pass from the
idea of weight to that of mass, and how we establish the doctrine of the
constancy of mass. We shall then give some account of the measurement
of gravity at the surface of the earth, and of the gravitation which is a
property of all matter wherever situated. We shall then proceed to the
di^cussion of those properties of matter which are perhaps best described
as involving change of form.
Weig'ht. — All matter at the surface of the earth has weight, or is
pulled towards the ground. The fact that the pull is to the earth at
all parts of its surface shows conclusively that it is due to the earth.
Apparent exceptions, such as the rising of a balloon in air, or of a cork
in water, are of course explained, not by the levity of the rising bodies,
but by the greater gravity of their surroundings. Oommon experience
A
f PROPERTIES OF MATTER,
with the balance shows that the ratio of the weights of two bodies is
constant wherever they are weighed, so long as they are both weighed
at the same point. Common experience shows too that the ratio is the
same however the bodies be turned about on the scale-pan of the balance.
The balance does not tell us anything as to the constancy of weight of
a given body, but only as to the constancy of ratio ; for if the weights of
ditlerent bodies varied, and the variation was always in the same ratio, the
balance would fail to indicate it. But here experiments with pendulums
supplement our knowledge. A given pendulum at a constant temperature
and in a fixed position has, as nearly as we can observe, the same time of
8win<' from day to day and from year to year. This implies that the
pull of the earth on the bob is constant — i.e., that the weight at the
same place remains the same.
This constancy of weight of a body at the same point appears to hold
whatever chemical or physical changes the matter in it may undergo.
Experiments have been made on the weight of sealed tubes containing
two substances which were at first separated, and which were then
mixed and allowed to form new chemical compounds. The tubes were
weio-hed before and after the mixture of their contents. But though
Landolt* and Heydweillerf have thought that the variations which they
observed were real and not due to erroi"S of experiment, Sanford and
Ray j have made similar experiments, and considered that the variations
were observational errors. Where variations have been observed they are
so minute and so irregular that we cannot as yet assume that there is any
change in weight.
Again, temperature does not appear to affect weight to any appreciable
extent. It is extremely difficult to make satisfactory weighings of a body
at two different temperatures. Perhaps the best evidence of constancy is
obtained from the agreement in the i-esults of diflferent methods of
measuring liquid expansion. In Dulong and Petit's U-tube method of
determining the expansion of mercury, two unit columns have different
heights but equal weights, and it is assumed that the cold column would
expand into the hot column without change of weight. But in the
dilatometer method nearly the whole expansion is directly measured, and
only the small expansion jf the envelope, measured by assuming the expan-
sion of mercury, introduces the assumption of constancy of weight with
change of temperature. The close agreement of the two methods shows
that there is no large variation of weight with temperature.
We may probably conclude that, up to the limit of our present powers
of measurement, the weight of a body at a given point is constant under
all conditions.
But when we test the weight at different points this constancy no
longer holds. The common balance used in the ordinary way fails to show
variation, since both pans are equally affected.
But very early in the history of the pendulum, as we shall show in the
next chapter, experiments proved that the seconds pendulum had different
lengths at different places, or that the same pendulum had different times
of swing at different places. In other words, the weight of the bob varied.
Thus a body is about 1 in 300 heavier at London than at the Equator.
* Zeit.f. Physik. Ckem., xii. 1, 1894.
+ Zcil.f. Physik., August 25, 1900, p. 527.
J Phys. liev., v, 1897, p. 247,
WEIGHT AND MASS. «
As early as 1662 an experiment was made by Dr. Power* in which a
variation of weight with change of level over the same point was looked
for. A body was weighed by a fixed balance, being first placed in the
scale-pan and then hung far below the same pan by a string. The
experiment was repeated by Hooke, and later by others, but tlie variation
was quite beyond the range of observation possible with these early
experimenters, and the results they obtained were due to disturbances in
the surroundings. I'lie first to show that the balance could detect a
variation was von Jolly (chap. iii. p. 41), who in 1878 described an
experiment in which he weighed a kilogramme on a balance 5"5 metres
above the floor and then hung the kilogramme by a wire so that it was
near the flooi". He detected a gain in the lower position of 1'5 mgm.
Later he repeated the experiment on a tower, a 5 kgm. weight gaining
more than 31 mgms. between the top of the tower and a point 21 metres
below. More recently Richarz and Krigar-Menzel found a variation
in the weight of a kilogramme when lowered only 2 metres (chap, iii.
P-^2-) ...
The evidence then is convincing that the weight of a body varies from
point to point on the earth's surface, and also varies with its distance above
the same point.
The question now arises — Is there any measurable quality of matter
which remains the same wherever it is measured ? Experiment showa
that there is constancy in that which is termed the mass of matter.
Mass. — Without entering into any discussion of the most appropriate
or most fundamental method of measuring force, we shall assume that wo
can measure forces exerted by bent and stretched spiings and similar con-
trivances independently of the motion they pioduce. We shall assume
that, when a given strain is observed in a spring, it is acting with a definite
force on the body to which it is attached, the force being determined by
previous experiments on the spring. Let us imagine an ideal experi-
ment in which a spring is attached to a certain body, which it pulls
horizontally, under constraint free from friction. Let the spring be
always stretched to a given amount as it pulls the body along, so acting
on it with constant force. Then all experiments and observations go to
show that the body will move with the same constant acceleration wherever
the experiment is made. This constancy of accelei-ation under a given
force is expressed by saying that the mass of the body is constant, i
Though the experiment we have imagined is unrealisable, actual experi- '
ments on the same lines are made for us by good chronometers. The
balance-wheel of a chronometer moves to and fro against the resistance
of the hair-spring, and its accelei'ation is very accurately the same for the
same strain of the spring at the same temperature in different lati-
tudes. The weight of the balance-wheel decreases by 3 in 1000 if the
chronometer is carried from London to the Equator. If the acceleration
under given force increased in the same ratio the rate of the chronometer
would change by 3 in 2000, or by two minutes per day, and the
chronometer would be useless for determinations of longitude. Again, a
tuning-fork, making, say, 256 vibrations per second at Paris at 16° will
have very accurately the same frequency at the same temperature wherever
tested. The same portion of matter in the prongs has the same acceleration
for the same strain and, presumably, for the same force all the world over.
* Mackenzie, The Laws of Gravitation, p. 2.
4 PROPERTIES OF MATTER.
This constancy of accelerAtion of a given body under given force holds
true likewise whatever the nature of the body exerting the force may be—
i.e., whether it be a bent spring, a spiial spring, air pressing, a string
puUing, and so on.
Further experiment shows that the acceleration of a given body is
proportional to the force acting on it. Thus, in a very small vibration of
a pendulum the fraction of the weight of the bob tending to restore it to
its central position is proportional to the displacement, and the simple
harmonic type of the motion with its isochronism shows at once that the
acceleration is proportional to the displacement, and therefore to the force
acting. When a body vibrates up and down at the end of a spiral spring
we attain have simple harmonic motion with acceleration proportional to
the distance from the position of equilibrium. The variation in the force
exerted by the spring is also proportional to this distance, or acceleration
is proportional to force acting. Indeed, elastic vibrations with their
isochronism go, in general, to prove this proportionality. If, then, we
accept the view that we can think of forces acting on bodies as being
measurable independently of the motion which they produce — measui\able,
say, by the strain of the bodies acting — we have good experimental proof
that a f^iven portion of matter always has equal acceleration under equal
force, and that the accelerations under different forces are proportional to
the forces acting upon it.
We can now go a stop farther and use the accelerations to compare
different masses.
Definition ofMSiSS.—The masses of bodies are p'oportional to the forces
producing equal accelerations in them.
An equivalent statement is, that the masses are inversely as the
acceleration produced by equal forces. It follows from our definition that,
if equal accelerations are observed in different bodies, then the masses are
proportional to the forces acting.
Observation and experiment further enable us to say that :
The masses of bodies are 2'>^'opoi'tional to their weights at the same jwint.
To prove this it is only necessary to show that all bodies have equal
acceleration at the same place when acted on by their weights alone — to
show, in fact, that the quantity always denoted by g is constant at the same
place.
A very simple though rough experiment to prove this consists in
tying a piece of iron and a piece of wood to the two ends of a thread and
putting the thread across a horizontal ring so that the two weights
depend at the same height above the floor. The thread is now burnt
in the middle of the ring and the iron and wood begin to fall at the same
in.stant. They reach the floor so nearly together that only a single
bump is heard. If the surfaces presented to the air are very different the
air resistance may interfere with the success of the experiment. But the
more the air resistance is eliminated the more nearly is the time of fall the
same. Thus, if a penny and a sheet of paper are placed on a board some
height above the floor, and if the board is suddenly withdrawn, the penny
falls straight while the paper slowly flutters down. Kow crumple up the
paper into a little ball and repeat the experiment, when the two reach the
ground as nearly as we can observe together.
Newton {Principia, Book III., Prop. G) devised a much more accurate
form of the experiment, using the pendulum, in which any difference of
WEIGHT AND MASS. 5
acceleration wouM be cumulative, and suspending in succession equal
weights of various kinds of matter. He saj's (Motte's translation) :
"It has been, now of a long time, observed by others, that all sorts of heavy
bodies (allowance being made for the inequality of retardation, which they
suffer from a small power of resistance in the air) descend to the Earth from
eqtiul heights in equal times ; and that equality of times we may distinguish to
a great accuracy, by the help of pendulums. I tried the thing in gold, silver,
lead, glass, sand, common salt, wood, water, and wheat. I provided two
wooden boxes, round and equal. I filled the one with wood, and suspended an
equal weight of gold (as exactly as I could) in the centre of oscillation of the
other. The boxes hanging by equal threads of eleven feet, made a couple of
pendulums perfectly equal in weight and figure, and equally receiving the
resistance of the air. And placing the one by the other, I observed them to
play together forwards and backwards, for a long time, with equal vibrations.
And therefore the quantity of matter in the gold (by Cor. 1 and 6, prop. 24,
book 2) was to the quantity of matter in the wood, as the action of the motive
force (or vis motrix) upon all the gold, to the action of the same upon all the
wood ; that is, as the weight of the one to the weight of the other. And the
like happened in the other bodies. By these experiments, in bodies of the same
weight, I could manifestly have discovered a difference of matter less than a
thousandth part of the whole, had any such been."
Newton here uses "quantity of matter" where we should now say
"mass." Bessel {Berlin Ahh., 1830, Ann. Fogg., xxv. 1832, or
Memoires relatifs a la Physique, v. p. 71) made a series of most careful
experiments by Newton's method, fully confirming the conclusion that
weight at the same place is proportional to mass.
Constancy of Mass. — The experiments which have led to the con-
clusion that weight at the same place is constant now gain another
significance. They show that the mass of a given portion of matter is
constant, whatever changes of position, of form, or of chemical or physical
condition it may undergo.
When we " weigh " a body by the common balance, say, by the
counterpoise method, we put it on the pan, counterpoise it, and then
replace it by bodies from the set of " weights " having an equal weight.
But our aim is not to find the weight of the body, the pull of the
earth on it. We use the equality of weight possessed by equal masses at
the same point of the earth's surface to find its mass. In buying matter
by weight we are not ultimately concerned with weight but with mass,
and we expect the same mass in a pound of it whether we buy in London
or at the Equator. A set of weights is really a set of masses, and when
we use one of them we are using it as a mass throvigh its weight.
Unit of Mass. — We can make a definite unit of mass by fixing on
some piece of matter as the standard and saying that it contains one unit
or so many units. So long as we are careful that no portion of the
standard piece of matter is removed and that no addition is made to it,
such a unit is both definite and consistent.
In this country the unit of mass for commercial purposes is the piece of
platinum kept at the Standards Ofiice at Westminster, marked " P.S.
1844 1 lb." and called the Imperial Avoirdupois Pound. But for scientific
purposes all over the world the unit of mass is the gramme, the one-
thousandth part of the mass of the piece of platinum-iridivim called the
•' Kilogramme-International," which is kept at Paris. Copies of this
kilogramme, compared either with it or with previous copies of it, are now
distributed through the world, their values being known to less, perhaps,
6 PROPERTIES OF MATTER.
than 0-01 mgm. For example, the copy in the Standards Office at Wes4
minster is certified to be
1-000000070 kgm.
with a prohal)le error of 2 in the last place.
According to a comparison carried out in 1883, the Imperial pound
contains
453"5924277 grammes,
though Parliament enacted in 1878 that the pound contained
453 •59245 grammes.
Of cour.se one piece of matter only can be the standard in one .system of
measurements, and the enactment of 1878 only implies that we should us6
a diffei-ent value for the kilogramme in England from that used in Franca
The diflerence is, however, (j^uitenegligible for commercial purposes.
CHAPTER II.
THE ACCELERATION OF GRAVITY. ITS VARIATION AND
THE FIGURE OF THE EARTH.
Contents. — Early History — Pendulum Clock — Picard's Experiments — Huygens'
Theory — Newton's Theory and Experiments — Bouguer's Experiments — Ber-
nouilli's Correction for Arc — Experiments of Borda and Cassini — Eater's Con-
vertible Pendulum — Bessel's Experiments and his Theory of the Reversible
Pendulum — Repsold's Pendulum — Yielding of the Support — DefEorges' Pendulum
— Variation of Gravity over the Earth's Surface — Richer — Newton's Theory of
the Figure of the Earth — Measurements in Sweden and Peru^ — Bouguer's
Correction to Sea-level — Clairaut's Theorem — Kater and Sabine — Invariable
Pendulum — Airy's Hydrostatic Theory — Faye's Rule — Indian Survey — Formula
foig in any Latitude — Von Sterneck's Half-second Pendulums — His Barymeter
— Gravity Balance of Threlfall and Pollock.
We shall describe in this and the following chapter the methods of
measuring two quantities ; the acceleration of falling bodies due to the
earth, at its surface (the quantity always denoted by g) ; and the accelera-
tion due to unit mass at unit distance (the quantity known as the gravita-
tion constant and denoted by G). The two may be measured quite in-
dependently, but yet they are closely related in that g is the measure of a
particular case of gravitation, while G is the expression of its general
measure. The two together enable us to find the mass and therefore the
mean density of the earth.
The Acceleration of Gravity.* — We shall briefly trace the history
of the methods which have been used in measuring g, for in so doing we
can set forth most clearly the difiiculties to be overcome and realise the
exactitude with which the measurement can now be made. We shall
then give some account of the experiments made to determine the varia-
tions of gravity and the use of the knowledge so gained to determine the
shape of the earth.
Early History. — The first step in our knowledge of the laws of
falling bodies was taken about the end of the sixteenth century, when
Stevinus, Galileo, and their contemporaries were laying the foundations
of the modern knowledge of mechanics. Stevinus, the discoverer of the
Triangle of Forces and of the theory of the Inclined Plane, and Galileo,
* A collection of the most important original papers on the pendulum
constitutes vols. iv. and v. of Memoircs relatifs a la Physique. It is prefaced by an
excellent history of the subject by M. Wolf, and contains a bibliography. The fifth
volume of The G. T. Survey of India consists of an account of the pendulum
operations of the survey, with some important memoirs. In the Journal de
Physique, vii. 1888, are three important articles by Commandant Defforges on the
theory of the pendulum, concluding with an account of his own pendulum. The
description given in this chapter is based on these works.
8 PROPERTIES OF MATTER.
the founder of Dynamics, were both aware that the doctrine then held that
bodies fall with rapidity pioportional to their weight was quite false, and
they asserted that under the action of their weight alone all bodies would
fall at equal rates. They pointed out that the diflerent rates actually
observed were to be ascribed to the resistance of the air, which has a
greater effect on the movement of light than of heavy bodies of e(]ual
size. Galileo made a celebrated experiment to verify this fact by dropping
bodies of different weights from the top of the Leaning Tower of Pisa,
and showing that they reached the ground in the same time. The air-
pump was not yet invented, so that the later verification by the "guinea
and feather " was not then possible. But Galileo did not stop with this
experiment, lie made the progress of dynamics possible by introducing
the conception of equal additions of velocity in equal times — the con-
ception of uniform acceleration. His first idea was that a constant force
131-ould give equal additions of velocity in equal distances traversed, but
investigation led him to see that this idea was untenable, and he then
enunciated the liypothesis of equal additions in equal times. He showed
that, by this hypothesis, the distance travei^sed is proportional to the
square of the time. Not content with mere mathematical deductions,
he made experiments on bodies mov^ing down inclined planes, and demon-
strated that the distances traversed were actually proportional to the
squares of the times — i.e., that the acceleration was uniform. By ex-
periments with pendulums falling through the arc of a circle to the
lowest point, and then rising through another arc, he concluded that the
velocity acquired in falling down a slope depends only on the vertical
height fallen through and not upon the length of the slope, or, as we
should now put it, that the acceleration is proportional to the cosine of
the angle of the slope with the vertical. He thus arrived at quite sound
ideas on the acceleration of falling bodies and on its uniformity, and from
his inclined plane experiments could have obtained a rough approxi-
mation to the quantity we now denote by g. But Galileo had no accurate
method of measuring small periods of time in seconds. The pendulum
clock was not as yet invented, and he made merely relative measurements
of the time intervals by determining in his experiments the quantity
of water which flowed through a small orifice of a vessel during each
interval.
To Galileo we also owe the foundation of the study of pendulum
vibrations. The isochronism of the pendulum had been previously ob-
served by others, but Galileo rediscovered it for himself, and showed by
further experiment that the times of vibration of diflerent simple pendu-
lums are proportional to the square roots of their lengths. He also used
the pendulum to determine the rate of beating of the pulse and recognised
the possibility of employing it as a clock regulator. He did not publish
liis ideas on the construction of a pendulum clock, and they were only
discovered among his papers long after his death.
From Galileo, therefore, we derive the conception of the appropriate
quantity to measure in the fall of bodies, the acceleration, and to him we
owe the instrument which as a free pendulum gives us the acceleration of
fall, and, as a clock regulator, provides us with the best means of deter-
mining the time of fall.
Soon after Galileo's death, Mersenne made, in 1644, the first determi-
nation of the length of a simple pendulum beating seconds, and a littla
THE ACCELERATION OF GRAVITY. 9
later he suggested as a problem the determination of the length of a
simple pendulum equivalent to a given compound pendulum.
Pendulum Clock. — But it was only with the invention of the
pendulum clock by Huygens in 1G57 that the second became an interval
of time measurable with consistency and ease. At once the new clock was
widely used. Its rate could easily be determined by star observalions, and
determinations of the length of the seconds pendulum by its aid became
common.
Picard's Experiment. — In 1GC9 Picard determined this length at
Paris, using a copper ball an inch in diameter suspended by an aloe fibre
from jaws. This suspension was usual in early work, the aloe fibre being
unaffected to any appreciable extent by moisture. Picard's value was
36 inches 8-| lines Paris measure. The Paiis foot may be taken as
■ii^ or 1"0G5 English feet, and there are 12 lines to the inch, so that the
length found was 39'09 English inches. Picard states that the value had
been fovmd to be the same at London and at Lyons.
Huygfens' Theory. — In 1673 Huygens propounded the theory of the
cycloidal pendulum, proving its exact isochronism, and he showed how to
construct such a pendulum by allowing the string to vibrate between
cycloidal cheeks. He determined the length beating seconds at Paris,
confii'ming Picard's value, and from the formula which we now put in the
form g = 7rH he found | the distance of free fall in one second, the
quantity which was at fii'st used, instead of the full acceleration we now
employ. His value was 15 ft. 1 in. 1^ lines, Paris measure, which would
give ^ = 32-16 Enghsh feet.
Huygens at the same time gave the theory of uniform motion in a
circle and the theory of the conical pendulum, and above all in importance
he founded the study of the motion of bodies of finite size by solving
Mersenne's problem and working out the theory of the compound
pendulum. He discovered the method of determining the centre of
oscillation and showed its interchangeability with the centre of suspension.
Newton's Theory and Experiments.— Newton in the Princijna
made great use of the theory of the pendulum. He there for the first
time made the idea of mass definite, and by his pendulum experiments
{Principia, sect, vi.. Book IL, Prop. 24), he proved that mass is
proportional to weight. He used pendulums too, to investigate the
resistance of the air to bodies moving through it, and repeated the
pendulum experiments of Wren and others, by which the laws of impact
had been discovered. But his great contribution to our present subject
was the demonstration, by means of the moon's motion, that gravity is
a particular case of gravitation and acts according to the law of inverse
squares, the attracting body being the earth. In Book III., Prop. 4, he
calculates the acceleration of the moon towards the earth and shows that,
starting from rest with this acceleration, it would fall towards the earth
15 ft. 1 in. 1^ lines (Paris) in the first minute. If at the surface of the
earth 60 times nearer the acceleration is 60^ times greater the same
distance would here be fallen through in one second, a distance almost
exactly that obtained by Huygens' experiments.
In a later proposition (37) he returns to this calculation, and now,
assuming the law of inverse squares to be correct, he makes a more exact
determination of the moon's acceleration, and from it deduces the value
10 PROPERTIES OF MATTER.
of gravity at the mean radius of the earth in latitude 45". Then by hiiS
theory of the variation of gravity with latitude, of which we shall give
Boine account below, he finds the value at Paris. He corrects the value
thus found for the centrifugal force at Paris and (in Pi*op. 19) for the
air displaced, which he takes as fxJjnj of the weight of the bob used in the
pendulum experiments, and finally arrives at 15 ft. 1 in. 1^ lines (Paris),
difiering from ITuygens' value by about 1 in 7500.
Boug'Uer's Experiments. — Though Newton was thus aware of the
need of tiie correction for the buoyancy of the air, it does not appear to
have been applied again until Bouguer made his celebrated experiments
in the Andes in 1787. These are especially interesting in i-egard to
the variations of gravity, but we may here mention some important
points to which Bouguer attended. While his predecessors probably
altered the length of the pendulum till it swung seconds as exactly
as could be observed, Bouguer introduced the idea of an *' invariable
pendulum," making it always of the same length and observing how long
it took to lose so many vibrations on the seconds clock. For this purpose
the thread of the pendulum swung in front of a scale, and he noted the
time when the thread moved past the centi-e of the scale at the same
instant that the beat of the clock was heard. Here we have an elementary
form of the " method of coincidences," to be described later. He used,
not the measured length from the jaw suspension to the centre of the bob,
which was a double truncated cone, but the length to the centre of oscilla-
tion of the thread and bob, and he allowed for change of length of his
measui'ing-rod with temperature. He also assured himself of the coinci-
dence of the centre of figure Avith the centre of gravity of the bob by
showing that the time of swing was the same when the bob was inverted.
He determined the density of the air by finding the vertical height through
which he must carry a barometer in order that it should fall one line, and
he thus estimated the density of the air on the summit of Pichincha at
■^-j^ ^ ^^ „ that of the copper bob of his pendulum. Applying these correc-
tions to his observations he calculated the length of the seconds pendulum
in vacuo.
Correction for Arc. — In 1747, D. BernouilH showed how to correct
the observed time of vibration to that for an infinitely small arc of swing.
The observed time is to a first approximation longer than that for an
2
infinitely small arc in the ratio 1 + -7; where a is the amplitude of the
16
angle of swing. The correction has to be modified for the decrease in
amplitude occurring during an observation.
Experiments of Borda and Cassini.— The next especially note-
worthy experiments are those by Borda and Cassini made at Paris in 1792
in connection with the investigations to determine a new standard of
length, when it was still doubtful whether the seconds pendulum might
not be preferable to a unit related to the dimensions of the earth. The
form of pendulum which they used is now named after Borda. It con-
sisted of a platinum ball nearly 1^ inches in diameter, hung by a fine iron
wire about 12 Paris feet long. It had a half-period of about two seconds
The wire was attached at its upper end to a knife edge — the advantages of
a knife-edge suspension having been already recognised — and the knife
edge and wire-holder were so formed that their time of swing alone was the
eame a.« that of the pendulum. In calculating the moment of inertia,
THE ACCEI.ERATION OF GRAVITY. ii
they could therefore be left out of account. At the lower end the wire
was attached to a shallow cup with the concavity downwards, and the ball
exactly fitted into this cup, being made to adhere to it by a little grease.
The ball could therefore be easily and exactly reversed without altering
the pendulum length, and any non-coincidence of centi-e of gravity and
centre of figure could be eliminated by taking the time of swing for each
position of the ball. The pendulum was hung in front of a seconds clock,
with its bob a little below the clock bob, and on the latter was fixed a
black paper with a white X-shaped cross on it. The vibrations were
watched through a telescope from a short distance away, and a little in
front of the pendulum was a black screen covering half the field. When
the pendulums were at rest in the field the edge of this screen covered
half the cross and half the wire. When the swings were in progress the
times were noted at which the pendulum wire just bisected the cross at the
instant of disappearance behind the screen. This was a " coincidence,"
and, since the clock bob made two swings to one of the pendulum, the
interval between two successive " coincidences " was the time in which the
clock gained or lost one complete vibration or two seconds on the wire
pendulum. The exact second of a coincidence could not be determined
but only estimated, as for many seconds the wire and cross appeared to
pass the edge together. But the advantage of the method of coincidences
was still preserved, for it lies in the fact that if the uncertainty is a
small fraction of the interval between two successive coincidences the
error introduced is a very much smaller fraction of the time of vibration.
For, suppose that the wire pendulum makes n half swings while the clock
makes 2« + 2. If the clock beats exact seconds the time of vibration of
the wire pendulum is
n \ n
If there is a possible error in the determination of each of two successive
coincidences of m seconds, or at the most of 2m in the interval of 2n + 2
seconds, the observed time might be
\ n±m/ ^ n\ ^nj' \ n^n^j
In one case Borda and Cassini employed an interval of 2n = 3000 seconds,
and found an uncertainty not more than 30 seconds for the instant of
coincidence. Thus
TO_ 30 _ 1
•n? 15U0' 75000
Now, as they observed for about four hours, or for five intervals in succes-
sion, the error was reduced to ^. or -i-, >qqq of the value of t. Practically
the method of coincidences determined the time of vibration of the
pendulum in terms of the clock time with sufficient accuracy, and the
responsibility for error lay in the clock. The pendulum was treated as
forming a rigid system, and the length of the equivalent ideal simple pen-
dulum was calculated therefrom. Corrections were made for air displaced,
for arc of swing, and for vaiiations in length with temperatvire.
The final value obtained was: Seconds pendulum at Paris = 4:i0-5593
12
PROPJ: IITIES OF MATTER.
. h
Qw
lines (Paris). As the metre = 44o-29G Paris lines, this gives 993-53 mm.,
and, corrected to soa-level, it gives l)90-85 mm.
Kater's Convertible Pendulum. — The difficulties in measuring the
length and in calculating the moment of inertia of the wire-suspended or
so-called .simple pendulum led Prony in 1800 to propo.se a pendulum
employing the principle of interchangeability of the centres of oscillation
and susfiension. The pendulum was to have two knife edges turned
inwards on opposite sides of the centre of gravity, so that it could be
swung from either, and was to be so adjusted that the time of
swing was the same in both cases. The di;stance between the
knife edges would then be the length of the equivalent simple
pendulum. Prony's proposal was unheeded by bis contemporaries,
and the paper describing it was only published eighty years later.*
In 1811, Bohnenberger made the same proposal, and again
in 1817 Captain Kater independently hit on the idea, and for
the first time carried it into practice, making his celebrated
determination of g at London with the form of instrument since
known as " Kater's convertible pendulum." This pendulum is
shown in Fig. 1 . On the rod are two adjustable weights, w and s.
The larger weight w is moved about until the times of swing
from the two knife edges ^-j k.^ are nearly equal, when it is
screwed in position. Then s is moved by means of a screw to
make the final adjustment to equality. Kater determined the
time of vibration by the method of coincidences, his use of it
being but slightly difierent from that of Borda. A white circle
on black paper was fastened on the bob of the clock pendulum ;
the convertible pendulum was suspended in front of the clock,
and when the two were at rest the tail-piece t of the former just
^h covered the white circle on the latter as viewed by a telescope a
^^B||. ^ few feet away. A slit was made in the focal plane of the
^^^B|^ eyepiece of the telescope just the width of the images of the
^^^^^ white patch and of the pendulum tail. A coincidence was the
instant during an observation at which the white circle was
quite invisible as the two pendulums swung past the lowest
point together. A series of swings were made, first from one
knife edge and then from the other, each series lasting over
four or five coincidences, the coincidence interval being about
500 seconds. The fine weight was moved after each series till
the number of vibrations per twenty-four hours only diflered by
a small fraction of one vibration whichever knife edge was used,
and then the ditierence was less than errors of observation, for
the time was sometimes greater from the one, sometimes greater from the
other. The mean time observed when this sta<:e was reached was corrected
for amplitude, and then taken as the time of the simple pendulum of
length equal to the distance between the knife edges, this distance being
carefully measured. A correction Avas made for the air displaced on tha
assumption that gravity was diminished thereby in the ratio of weight of
pendulum in air to weight of pendulum in vacuo. The value was then
corrected to sea-level. The final value of the length of the .seconds pendulum
at .sea-level in the latitude of London was determined to be 39'13'J2U inches.t
* Miinoircs relati/s a la Physique, iv. \i. G5.
t The experiments are described iu a paper in the Phil. Trans, for 1818 "An
Fig. 1.—
Katc'i-'s
Convertible
I'eudulutu.
THE ACCELERATION OF GRAVITY. 13
Bessel's Experiments and his Theory of the Reversible
Pendulum. — In 182G Jiessel made experiments to determine the length
of the seconds pendulum at Koenigsberg. He used a wire-suspended
pendulum, swung first from one point and then from another point,
exactly a "Tuiseof Peru"* higher up, the bob being at the same level in
each case. Assuming that the pendulums are truly simple, it will easily be
seen that the difterence in the squares of the times is the square of the
time for a simple pendulum of length equal to the difference in lengths,
and therefore the actual length need not be known. But the practical
pendulum departs from the ideal simple type, and so the actual lengths
have to be known. As, however, they enter into the expression for the
difierence of the squares of the times, with a very small quantity as co-
efficient, they need not be known with such accuracy as their diflerences.
Bessel took especial care that this difference should be accurately equal to
the toise. At the upper end, in place of jaws or a knife edge, he used a hori-
zontal cylinder on which the wire wrapped and unwrapped. He introduced
corrections for the stiffness of the wire and for the want of rigidity of
connection between bob and wire. The necessity for the latter correction
was pointed out by Laplace, who showed that the two, bob and wire, could
not move as one piece, for the bob acquires and loses angular momentum
around its centre of gravity, which cannot be accounted for by forces
passing through the centre, such as would alone act if the line of the wire,
produced, always passed through the centre. In reality the bob turns
through a slightly greater angle than the wire, so that the pull of the wire
is now on one side and now on the other side of the centre of gravity.
The correction is, however, small if the bob has a radius small in comparison
with the length of the wire.
If I is the length of the wire, r the distance of the centre of gravity of
the bob from the point at which the wire is attached to it, and k the radius
of gyration of the bob about an axis through the centre of gravity ; then,
neglecting higher powers than k^ the equivalent simple pendulum can be
shown to be
I + r r{l + rf
the last term being due to the correction under consideration. As an
illustration, suppose the bob is a sphere of 1 inch radius and the wire
is 38 inches long ; then the equivalent simple pendulum in inches is
39 + •010256 + -000102, and the last term, 1/400000 of the whole length,
need only to be taken into account in the most accurate work.
Bessel also made a very important change in the air correction. The
effect of the air on the motion may be separated into three parts —
(1) The buoyancy, the weight of the pendulum being virtually
decreased by the weight of the air which it displaces.
(2) The flow of the air, some of the air moving with the pendulum,
and so virtually increasing its mass.
account of experiments for determining the length of the pendulum vibrating
seconds in the latitude of London," and in a paper in the Phil. Trans, for 1819,
" Experiments for determining the variations in the length of the pendulum
vibrating seconds," Kater applies further corrections and gives the above value.
* The " Toise of Peru " was a standard bar at the Paris Observatory, 6 Paris feet
or about J949 millimetres long.
14 PROPERTIES OF MATTER.
(.3) The air drag, a viscous resistance which comes into play between
the diflerent layers of air, moving at ditferent rates, a resistance trans-
mitted to the pendulum.
As far back as 17SG Du Buat had pointed out the existence of the
second effect, and had made experiments with pendulums of the same
lenijth and form, but of different densities, to determine the extra mass for
various shapes. Bessel, not knowing Du Buat's work, reinvestigated the
matter, and again by the same method determined the virtual addition to
the mass for various shapes, and among others for the pendulum he used.
The viscous resistance was first placed in its true relation by Stokes'
investigations on Fluid Motion in 1847. In pendulum motion we may
regard it as tending to decrease the amplitude alone, for the effect on the
time of vibration is inappreciable. We may represent its effect by
introducing a term proportional to the velocity in the equation of motion,
which thus becomes
d + rd+fid^O
The solution of this is 0 = Ae ~ ^cos j \ fi -~t- a \
where A and a are con.stants.
9
The period is T =» — ^---__ where v depends on the viscosity.
Approximately! = —ll + —\ or the time is increased by the
viscosity in the ratio 1 + -|1 : 1,
or since fi = -y^ (nearly), in the ratio 1 + : 1.
To see the order of this alteration, suppose that p^ p^ represent two
succeeding amplitudes on opposite sides of the centre — i.e., values for which
5' = 0, or cos ( "^ '^ J " .7')^^' then p, = eT or, taking logarithms,
iogf^'=x=?:?
Now in one of Eater's experiments the arc of swing decreased in
about 500 seconds from 1-41° to 1 -18°, or in the ratio MDo : 1.
Then /PiV''^ 1-195 and 500X=log,M95 = 0-178
whence X = -000356 and -^ = 2^J_ = 6 x 1 0-» about.
In Borda's pendulum the elFect was about the same — i.e., one that ia
practically quite negligible.
THE ACCELERATION OF GRAVITY. 15
Bessel also used the pendulum to investigate afresh the correctness of
Newton's proof that mass is proportional to weight, carrying out a series
of experiments which still remain the best on the subject. But Bessel's
chief contribution to gravitational research consisted of his theory of the
'* reversible pendulum." He showed that if a pendulum were made
symmetrical in external form about its middle point, but loaded at one
end, to lower the centre of gravity, and provided with two knife edges,
like Kater's pendulum, one very nearly at the centre of oscillation of the
other, the length of the seconds pendulum could be deduced from the
two times without regard to the air efiects. Laplace had shown that the
knife edges must be regarded as cylinders, and not mere lines of suppoit.
Bessel showed, however, that if the knife edges were exactly equal
cylinders their efiect was eliminated by the inversion, and that if they were
different cylinders their effect was eliminated by interchanging the knife
edges, and again determining the times from each — the " erect " and
*' inverted " times as we may conveniently term them.
We shall consider these vai'ious points separately.
In the first place, Bessel showed that it was unnecessary to make the
erect and inverted times exactly equal. For if Tj and T^ be these times,
if Aj h^ be the distances of the centre of gravity from the two knife edges,
and if k be the radius of gyration round an axis through the centre of
gravity, the formula for the compound pendulum gives
Multiply respectively by h^, A^, subtract and divide by h^ - h^ and w9
have
Let us put "' } fiii- = T^
We shall term T the computed time. We see that it is the time corresponding
to a length of simple pendulum Aj + h^ It may be expressed in a more
convenient form, thus :
Let T2 = ii-±i:^ and a^ = ii_-i2. ,
2 2
then Tj- = r- + «', T/ == t- - a^, and substituting in T^ we get
_ A,T,^ - A3T/ _^,^^^,K + h,_ T,^ + T/ ^ T,^ - T/ h, + h.
Now h^ + K is measurable with great exactitude, but Aj and Aj, and
therefore A, - A.„ cannot be determined with nearly such accuracy. The
method of measuring them consists in balancing the pendulum in horizontal
position on a knife edge and measuring the distance of the balancing knife
edge from each end knife edge. But the formula shows that it is not
necessary to know A, - h., exactly, for it only occurs in the coefficient of
T,- - T/, which is a very small fraction of T,^ + T/. Knowing, then, A, + A,
exactly and A, - h^ approximately, we can conjpute the time corresponding to
16
PROrKRTIES OF MATTER.
h^ + Aj from the times in theei-ect and inverted positions and avoid the trouble-
some series of trials which Kater made before obtaining exact equality for
them from each knife edge.
Now let us consider the air effect. Take first the erect position of the
pendulum. We may represent the buoyancy by an upward force applied
at the centre of gravity of the displaced air, and equal to its weight iwj.
Let tliis centime of gravity be distant s from the centre of suspension.
The mass of air flowing with the pendulum will have no effective weight,
since it is buoyed up by the surrounding air. It is merely an addition to
the mass moved and serves to increase the moment of inertia of the
pendulum. Let us represent it by the addition of a term m'd- when the
pendulum is erect.
Then we have ^^\ - ^^^V + ^) + "^'^^^ - ^^^^' t f) + "^'^^Yl +."'^
47r-
MA, — ms
M/i.
MA,
Aj" + K' Aj
K
- + <• ms md?
m
neglecting squares and products of ~ and
MA,
^, since in practice these
quantities are of the order 10"*.
Now invert and swing from an axis near the centre of oscillation.
The value of m is the same, but its centre of gravity may be at a different
distance from the new suspension, say s'. The air moving may be different,
so that we must now put m"d'- instead of m'd'\ We have then
9V
47r»
_A/ + «^_^AJ
A„
+ (c- ms
~~ma:
A,
+
m"<P
MAT
If we put hJi.^ = K- as an approximation in the coefficients of the
m
small terms containing — the computed time T is given by
4«^
477-
A,T,-
AX
2\
K
■.h^ + h.^ + h + ^'-^ '"''
ms' (vi - m")d?
Aj - A, M M(Aj - A,)
But if we make the external form of the
pendulum symmetrical about its middle point,
so that the two knife eilges are equidistant
from the centre of figure, then s = s' and m
■ m
and JLt= = A, + A,
iTT
Fio. 2. — Effoct of cylindrical
Form of Knife Edge.
Then the air efTect is eliminated in the
computed time. It is necessary here that the
barometer and thermometer should give the
same readings in each observation ; if not,
corrections must be made ; but, as they will be
very small, an exact knowledge of their value is
unnecessary.
In investigating the effect of the cylindrical
form of the knife edges we shall for simplicity
suppose them each to have constant curvature,
THE ACCELERATION OF GRAVITY. 17
the radius of the erect one being p^, that of the inverted one p^. If C, Fig. 2,
is the centre of curvature of the knife edge, 0 the point of contact, G the
centre of gravity, then CG =h^ + p^ and the work done is the same as if
G were moved in a circle of radius h^ + p^, since the horizontal travel of G
does not ."fleet the amount of work. The instantaneous centre of motion
is the point of contact 0. The kinetic energy is therefore
M(k2 + 0G=)|'
But OG2 = OC= + CG=-20CCGcos5
-pr + (Pi + ^h)^-Wp. + ^:)(l-|)^PProximatcly - (^ ^ '^''^ V U ' * "'
■1 h^^ neglecting p^h^O- and smaller quantities.
Then the kinetic energy is M(Aj- + k")- .
The work done from the lowest point is
M^ (A, + Pi) (1 - cos 6) = Mg {h, + p,) ^
Hence the erect time is given by *
gTlJ>l±l^hfj^L_p,\^^
47r* hi + Pi A, \ hj
the inverted time is given by
47r h, \ K
In the computed time we may put K- = hfi^\n the coefficient of the small
quantities p, and p,, and therefore
7-5-73 — I — I — -^^1 + ^2 + 7 — r\p2 Pi)
47r2 47r-\ k^-h^ J K'K
Now interchange the knife edges. Assuming that no alteration is
made except in the interchange of p, and p^, the computed time T' is
given by
adding the two last equations together and dividing by 2,
47r- 2 ' '
* If in simple harmonic motion the kinetic energy at any point is i«5- and the
work from the centre of swing is Ihff-, then the periodic time is easily seen to be
'Wi
A
18
PROPERTIES OF MATTER.
Repsold's Pendulum. — Bessel did not himself construct a peudulum
to fulfil these conditions, but, after his death, llepsold in 1860 devised a form
with interchangeable knife edges and of symmetrical
form now known as Repsold's Reversible Pendulum
(Fig. 3), in which he carried out Bessel's suggestions.
The stand for the instrument was, perhaps fortunately,
far from sufficiently firm, for as the pendulum swung
to and fro the stand swung with it. Attention was
directed to the investigation of the source of error.
Its existence was already known, but its magnitude
was not suspected till Peirce and others showed how
seriously it might affect the time.
Yielding" of the Support. — The centre of gravity
moves as if all the forces acted on the whole mass
collected there, so that if we find the mass acceleration
of the centre of gravity, and subtract the weight,
Mg, we have the force due to the support. Reversing,
we have the force on the support.
The acceleration of the centre of gravity is h^d
along the arc and /i^d' towards the point of support.
Resolving these horizontally and vertically,
horizontal acceleration
= h^6 cos 6 - h^d' sin 6 = h^6 approximately ;
vertical acceleration
Fig. 3.— Repsold's Ee-
versibie Pendulum. = ^ ^sin 0 + hJ' COS 6 = hJd + hJ' approximately ;
The Russian Pen- ' ' i i i r j t
duluin used in the
Indian Survey.
but ^= -
gh^e
Then the horizontal force on the stand is M^ — ' — 0
h{ + K^
= Mcr- — L_ since K- = h,h.,
If a is the amplitude of 0, then 6- = -^- {a- - 0=)
and the vertical force upwards, on the pendulum
Now in finding the yielding of the stand we only want the varying
part of this. Reversing it, the variation in the force on the stand
which is of the second order in 0, and it can be shown that the effect on
the time of swing is negligible in comparison with that of the horizontal
yielding.
THE ACCELERATION OF GRAVITY.
19
Let the yielding to a horizontal force be e per dyne. Let OC (Fig. 4)
be the vertical position, AG the position when displaced through ang'e 0.
m;?..
Then the yielding OA =e— — l
ge
ML
produce GA to 0', then OO' = OA/0 =e^— J-*7 = f^i say,
or the instantaneous centre is raised cZ, above O, and the
centre of gravity is moving in a circle of radius
Let the instantaneous centre be raised cL = e
when the pendulum is inverted.
Hence the erect time is given by
Fig. 4.— Yielding
of the Support.
4^ /ii + c^j h^ + d^
the inverted time by
4»» h, + d.
"2 ' ^"2
K + ^h
and the computed time by ^- = h^ + h^-\-eM.g, since h^d^ = \dy
We see that eM^ is the horizontal displacement of the support due to
the weight of the pendulum applied horizontally.
Defforgfes' Pendulums. — Starting from this point, Commandant
Deftbrges has introduced a new plan to eliminate the effect of yielding,
using two convertible pendulums of the Repsold type, of equal weight, of
different lengths, and with a single pair of knife edges, which can be trans-
ferred from one to the other. The ratio of /i, : A, is made the same for
each.
Let the radii of curvature of the knife edges be denoted by f), p^, let
Ji j^h_, = \ refer to the first pendulum, h\ + h'., = I.^ refer to the second.
The efiect of yielding is the Fame for each, increasing the length by 2.
Let T T' be their computed times,
then
and
K - K
20 PROPERTIES OF MATTER.
7 7 /
since -l = -i^ the co-efEcient of p^ - p, disappears, and it is not necessary
to interchange the knife edges on the same penduhim. Hence the pen-
dulums ai-e convertible, and we have
£-^(T^-T'0 = ?,-;,
The United States Coast and Geodetic Survey have recently constructed
a pendulum in which the planes are on the pendulum and the knife edges
on the support. The one disadvantage is the difficulty of so suspending
the pendulum that the same part of the plane is always on the knife edge,
but against this is to be set the probable greater accuracy of moasure-
meiit of ^1 + /tj and the freedom from the necessity of interchange of
knife edge. Further, should a knife edge be damaged it can be reground
without affecting the pendulum, whereas in the ordinary construction
regrinding really alters the pendulum, which practically becomes a
different instrument.
Variation of Gravity over the Surface of the Earth.
Richer. — The earliest observation showing that gravity changes with
change of place was made by Richer, at the request of the French
Academy of Sciences, in 1672. He observed the length of the seconds
pendulum at Cayenne, and returning to Paris found that the same
pendulum must there be lengthened \\ Paris lines, 12 to the inch.
Newton's Theory. — This observation waited no long time for an
explanation. Newton took up the subject in the Princ'qna (Book IH.,
Props. 18-20) and, regarding gravity as a terrestrial example of uni-
versal gravitation, he connected the variation with the form of the
earth. He showed first that if the earth is taken as a homogeneous
mutually gravitating fluid globe, its rotation will necessarily bring about a
bulging at the Equator, for some of the weight of the equatorial portion
■will be occupied in keeping it moving in its daily circle while the polar
part has but little of such motion. A column, therefore, from the centre
to the surface must be longer at the Equator than at the Pole in order
that the two columns shall pioduce equal pressures at the centre. Assimiing
the form to be spheroidal, the attraction will be different at equal distances
along the polar and equatorial radii. Taking into account both the
variation in attraction and the centrifugal action (o^-y- of gravity at the
Equator), Newton calculated the ratio of the axes of the spheroid. Though
his method is open to criticism, his result from the data used is perfectly
correct, viz., that the axes are as 230 : 229. Taking a lately measured
value of 1" of latitude, he found thence the radii, and determined their
difference at 17"! miles. He then found how gravity should vary over
such a sphei'oid, taking centrifugal action into account, and prepared
a table of tlie lengths of 1° of latitude and of the seconds pendulum
for every 5° of latitude from the Equator to the Pole. From his table
THE ACCELERATION OF GRAVITY.
21
the pendulum length at Cayenne, in latitude 4° 55', should be 1 line
less than at Paris in latitude 48° 50'. He assigns part of the difference
of this from the diminution of I-^ lines observed by Richer to expansion
of the scale with higher temperature near the Equator.
The Swedish and Peruvian Expeditions.— Newton's theory of
the figure of the earth as depending on gravitation and rotation led early
in the eighteenth centuiy to measurements of a degree of latitude in Peru
and in Sweden. If the earth were truly spheroidal, and if the plumb-
line were eveiywhere perpendicular to the surface, two such measurements
would sutiice to give the axes a and h, inasmuch as length of arc of 1°
= .(r-
f + 36sin'^^^3G00sinl" where 6 = ^^:
2 J a
the ellipticity and X X'
are the latitudes at the beginnincf and end of the arc*
^^'^e know now that through local variations in gravity the plumb-line
is not perpendicular to a true spheroid, but that there are humps and
hollows in the surface, and many measurements at difierent parts of the
earth are needed to eliminate the local variations and find the axes of the
spheroid most nearly coinciding with the real surface. But the Swedish
and Peruvian expeditions clearly proved the increase of length of a degree
in northerly regions, and so proved the flattening at the Poles. These
expeditions have another interest for us here in that pendulum observa-
tions were made. Thus Maupertuis, in the northern expedition, found
that a certain pendulum clock gained 59 "1 seconds per day in Sweden on
its rate in Paris, while Bouguer and La Condamine, in the Peruvian
expedition, found that at the Equator at sea-level the seconds pendulum
was 1"26 Paris lines shorter than at Paris. Bouguer's work, to which we
have already referred, was especially important in that he determined the
length of the seconds pendulum at three elevations : (1) At Quito, which
may be regarded as a tableland, the station being 14GG toises t above sea-
level ; (2) on the summit of Pichincha, a mountain rising above Quito to
a height of 2434 toises above sea-level; and (3) on the Island of Inca, on
the river Esmeralda, not more than thirty or forty toises above sea-level.
The Equator runs between Quito and the third station, and they are only
a few miles from it. In space free from matter rising above sea-level gravity
might be expected to decrease according to the inverse square law starting
from the earth's centre, so that if h is the height above sea-level and r is
station.
Above
Sea-level
in Toises.
Observed
Seconds
Pendulum
in Lines.
Correction
for Tem-
perature.
Correction
for
Buoyancy.
Corrected
Seconds
Pendulum.
Fraction
less than
at Sea-
level.
Fraction
jriven by
Inverse
Square
Law 2 hfr.
Pichincha .
Quito .
Isle of Inca
2434
14G6
438-70
438-83
430-07
-•05
-f-075
-I--04
-t--05
-f -06
438-69
438-88
439-21
TaST
1
* Airy, " Figure of Earth." Fncyc. Met., p. 192.
■|- The toise is 6 Paris feet, or 6-395 English feet.
22 PROPERTIES OF MATTER.
the earth's radius, the decrease should be ^hjr of the original value. In
the table on p. 21, Bouguer's results are given. In the last column but
one is the decrease observed at the upper stations, and in the last column
the decrease calculated by 2A/?'.
It will be seen that gravity decreased more slowly than by the inverse
square law. Centrifugal force would act in a contrary way, though, as
Bouguer showed, by a negligible amount. The excess of gravity, as
observed, above its value in a fi'ee space must therefore be assigned to the
attraction of the matter above the sea-level. Bouguer obtained for the
value of gravity g^ on a plateau of height h, as compared with its value at
sea -level g,
where I is the density of the plateau and A the density of the earth.
This formula, now known as Bouguer's Rule, seems to have dropped
out of sight till it was again obtained by Young in 1819, but on its
revival it was generally employed to reduce the observed value at a station
to the sea-level value in the same latitude.
Putting it in the form ?^ — ^ = !^/l _ ? i\
g, r\ 4. A/
3993
and using the values at Quito and sea-level, A= '. ' Z
850
Bouguer remarked that this result sufficed to show that the density of
the earth was greater than that of the Cordilleras, and consequently that
the earth was neither hollow nor full of water, as some physicists had
maintained. We now know that the value of A f^o obtained is far too great,
and shall see later what is the probable explanation.
CiairautS Theorem. — In 1713 Clairaut published his great treatise,
Theorie de la Figure de la Terre, which put the investigation of the figure of
the earth on lines which have ever since been followed. In this work he
takes the surface of the earth as a spheroid of equilibrium — i.e., such that a
layer of water would spread all over it, and assumes that the internal density
varies so that layers of equal density are concentric co-axial spheroids.
Denoting gravity at the Equator, Pole, and latitude X, by g^, g^, g\ respec-
tively, and putting in = centrifugal force at Equator jg^ and e = ellipticity =
difference of equatorial and polar radii / equatorial radius, he shows (1) that
where w is a constant : (2) that
From (1) and (2) we get
5'A = 5'.|l + Uw-ejsin-xj,
a result known as Clairaut's Theorem.
Laplace showed that the surfaces of equal density might have any
THE ACCELERATION OF GRAVITY. 23
nearly sphei-ical form, and Stokes [Math. Phys. Papers, vol. ii. p. 104),
going further, showed that it is unnecessary to assume any law of density
so long as the external surface is a spheroid of equilibrium, for the theorem
gtill remains true.
From Clairaut's Theorem it follows that, if the earth is an oblate
spheroid, its ellipticity can be determined from pendulum experiments on
the variation of gravity without a knowledge of its absolute value, except
in so far as it is involved in m. And if the theorem were exactly
true, two relative determinations at stations in widely different latitudes
should suffice. But here again, as with arc measurements, local variations
interfere, and many determinations must be made at widely scattered
stations to eliminate their effect.
Kater and Sabine. Invariable Pendulums.— During the last half
of the eighteenth century much pendulum work was carried on, but hardly
with sufficient accuracy to make the i-esults of value now, and we may con-
sider that modern research begins with Kater, who constructed a number of
"invariable pendulums," nearly beating seconds, and in shape much like
his convertible pendulum without the reverse knife edge. The principle
of " invariable pendulum " work consists in using the same pendulum at
different stations, determining its time of vibration at each, and correcting
for temperature, air effect, and height above sea-level. The relative values
of gravity are thus known, or the equivalent, the relative lengths of the
seconds pendulum, without measuring the length or knowing the moment
of inertia of the pendulum. Kater himself determined the length of the
seconds pendulum at stations scattered over the British Islands, and
Sabine, between 1820 and 1825, carried out observations at stations
ranging from the "West Indies to Greenland and Spitzbergen. About the
*ame time Freycinet and Duperry made an extensive series ranging far
into the Southern Hemisphere, and other observers contributed observa-
tions. Now, though different pendulums were used, these series over-
lapped and could be connected together by the observations at common
stations ; and Airy in 1830 (Encyc. Met., " Figure of the Earth ") deduced a
value of the ellipticity of about -g^-
Breaking down of Bouguer'S Rule. — Subsequent work brought
into ever-increasing prominence the local divergences from Clairaut's
formula, and it gradually became evident that on continents and on high
ground the value of gravity was always less than would be expected from
Clairaut's formula when corrected by Bouguer's rule, while at the sea
coast and on oceanic islands it was greater.
Indian Survey. — Thus, in the splendid series of pendulum ex-
periments carried out in connection with the Indian Trigonometrical
Survey between 1865 and 1875 [G. T. Survey of India, vol. v.) the
variations were very marked. In these experiments, invariable pen-
dulums, Kater's convertible and Eepsold's reversible pendulum were all
used, and observations were made by Basevi and Heaviside from More, on
the Himalayas, at a height of 15,427 feet, down to the sea-level. The series
was connected with others by swinging the pendulums at Kew before
their transmission to India, and very great precautions were taken to
correct for temperature, and the air effect was eliminated by swinging in
a vacuum. At More the defect of gravity was very marked.
Airy's " Hydrostatic " Theory. Faye's Rule.— Airy {PMl. Trans.,
1855, p. 101) had already suggested that elevated masses are really
21- PROPERTIES OF MATTER.
buoyed up by matter at their base lii^liter than the average ; that in fact
tliey float on the licjuid or more probably viscous solid interior very much
as icebergs float on the sea. If the high ground is in equilibrium, neither
rising nor falling, we may perhaps regard the total quantity of matter
underneath a station as being equal to that at a station at sea-level
in the same latitude. This hydrostatic theory has led Faye to suggest
that the term in Bouguer's rule should be I'eplaced by a term only
taking into account the attraction of the excess of matter under the
station above the average level of the near neighbourhood, a suggestion
embodied in Faye's rule.
llecent work by the American Survey {Amer. Joiirn. Science, March
1896, G. R. Putnam) has shown that on the American continent Faye's
rule gives results decidedly more consistent than those obtained from
Bouguer's rule.
By a consideration of the results obtained up to 1880 by the pen-
dulum, Clarke {Geodesy, p. 350) gives as the value of the ellipticity
e = — -— r, a value almost coincidintr with that obtained from measure-
2l2-2± 1-5 °
ments of degrees of latitude. Helmert, in 1884, gave as the result of
pendulum work , and we may now be sure that the value differs very
little from .
300 ^ .
Helmert {Theorieen der hoheren Geoddsie, Bd. II. p. 241) also gives
as the value of g in any latitude X,
g^ = 978-00(1 + 0-005310 sin' \)
and this may be taken as representing the best results up to the present.
Von Sterneck's Half-second Pendulums.— The labour of the
determination of minute local variations in gravity was much lessened by
the introduction by von Sterneck, about 1880, of half -second invariable
pendulums, and his improved methods of observation have greatly in-
creased the accuracy of relative determinations at stations connected by
telegraph.
With half the time of swing the apparatus has only one-fourth the
linear dimensions, and it can be made at once more steady and more
portable. The size of the pendulum being thus reduced — it is about
10 inches long — it can without much trouble be placed in a chamber which
can b3 exhausted and which can be maintained at any desired temperature.
Each pendulum can therefore be made to give its own temperature and air
corrections by preliminary observations. The form of the pendulum is
shown in Fig. 5. The chief improvements in the mode of observation
introduced by von Sterneck consist, 1st, in the simultaneous comparison
with the same clock of the swinging of two pendulums at two stations at
which gravity is to be compared. For this purpose the two stations are
connected by an electric circuit containing a half-seconds "break circuit"
chronometer, which sends a signil through each station every half-second,
and thus clock-rates are of little importance. And, 2nd, the method of
observing the coincidences of the pendulum with the chronometer signals.
In the final form this consists in attaching a small mirror on the pendulum
THE ACCELERATION OF GRAVITY.
25
knife edge (not shown in Fig. 5, which represents an earlier form) per-
pendicular to the plane of vibration of the pendulum, and placing a fixed
mirror close to the other and parallel to it whan the pendulum is at rest.
Pia. 5.
The chronometer signals work a relay, giving a horizontal s ">ark, and this
is reflected into a telescope from both mirrors. When the pandulum is at
rest the image of the spark in both mirrors appears on the horizontal
cross-wire, and when the pendulum is vibrating a coinciilenc3 occurs when
the two images are in this position. The method admits of exceedingly
26
PROPERTIES OF MATTER.
accurate determination. We shall see later how von Sterneck used the
method in fi^ravitation experiments. Here it is suflicient to say that he
has used it in many local determinations of gravity, nnd that his pendulums
have been used without the simultaneous method for determinations at
various stations in both hemispheres. The American Geodetic Survey has
adopted very similar apparatus and methods, and it appears probable that
we shall soon have a knowledge of the variation of gravity over the surface
of tlie earth of a far more detailed and accurate kind than could possibly
be obtained by the older methods.
Differential Gravity Meters. — Before invariable pendulums were
brought to their present accuracy and portability, there was some hope
that for relative determinations the pendulum might be superseded by a
statical measurer of gravity which would do away with the need for time
measurements. Such an instrument must essentially consist of a mass
supported by a spring, and the variation in gravity must be shown by the
alteiation in the spring due to the alteration in the pull of the earth on
the mass. The earlier instruments devised for the purpose need not be
described, for they were quite incapable of the accuracy attained by
invariable pendulums. The first instrument which promised any real
success was devised by von Sterneck, and Ls termed by him the Barymeter
{Mittheilangen des K. K. Militar-Geog. Inst., Wien, v. 1885).
Von Sterneck's Barymeter.
1 0 — A brass plate P (Fig. G), i5U cm. x
20 cm., is balanced on a knife edge, s.
Along a diagonal is a glass tube
terminating in bulbs 0 and U, 5 cm. x
6 cm., so that in the equilibrium
position 0 is about 25 cm. above U.
The tube and about i of each bulb
is filled with mercury, and above the
mercury is nitrogen. The apparatus
is adjusted so that at 0° C. and for
a certain value of gravity the edges
of the brass plate are horizontal
and vertical, a level W showing
when this position is attained. If now gravity were to increase, the
weight of the mercury would be greater, and it would tend to flow from O
and compress the gas in U. Thus the balance would tilt over to the left,
and the tilting still further increasing the pressure on U, the flow
downwards is increased. The instrument can thus be made of any
desired sensitiveness, and its deflections can be read by scale and measured
in the usual way. To compensate for changes of temperature, a second
tube terminating in smaller bulbs o and u, each about 6 cm. x 3 cm., is
fixed along the other diagonal. This contains some mercury, but above
the mercury in u is alcohol, and only o contains nitrogen. If the
temperature rises the mercury becomes less dense, and on this account it
is driven from U to O in the larger tube, but still more is it driven in this
du-ection from the fact that the increase of pressure of the gas in U is
greater than in O. Meanwhile, the alcohol in u expanding, drives the
mercury in the smaller tube into o, and by .suitable adjustments of volume
the two can be made to balance sufficiently for such small temperature
variations as will arise when the whole is placed in a box surrounded with
Von Sterneck's Barymeter,
THE ACCELERATION OF GRAVITY.
27
melting ice, and it is thus that the instrument is used. With this
instrument von Sterneck could detect the change in gravity in going from
the cellar of a building to a height of 25 metres.
Threlfall and Pollock's Quartz-thread Gravity Balance.—
In the ritil. Trans., A. r.)o, 18131), p. 215, Threlfall and l^llock describe an
instrument for measuring variations in gravity statically which is both
accurate and portable.
The essential features of the instrument are represented in Fig. 7.
A and B are two metal rods which can slide along their common
axis. C is a coach-spring attached to A . H I is a quartz thread 30-5 cm.
long and •0038 cm. in diameter stretched horizontally between B
and C. D is a piece of gilded brass wire soldered to the quartz thread.
Its weight is "018 gm., its length 5%S cm., and its centre of gravity is
a little to one side of the quartz thread. Its weight therefore tends
to pull it into the vertical position and twist the quartz. But such a twist
^
n
im
0"
a
[r~i
r\
a
G
^
tr
Fig. 7. — Tlirelfall and Pollock's Quartz-thread Gravity Balance.
can be put on the quartz thread by rotating the arm G, which cariies a
vernier, that D is brought into the horizontal position. For this about
three whole turns are required. The end of D when in the horizontal
position is on the cross-wire of the horizontal microscope E. The hori-
zontal position of the brass wire is only just stable. If it be twisted a few
degrees more the point of instability is reached and the wire tends to
continue moving round, and would do so but for an arrester. The mode
of using the instrument consists in determiuing the twist put on the quai'tz
thread by the arm G to bring it into the horizontal position. If gravity
increases, the moment of the weight of D increases and a greater twist is
required. To calibrate the insti'ument the change in reading of the vernier
on G is observed in passing from one station to another, at both of which
g is known — the two stations selected being Sydney and Melbourne. Of
course, temperature corrections are necessary both on account of the change
in length of D and the change in rigidity of the quartz. Preliminary
determinations of these were made at one station. For the details of the
instrument and the mode of using it we refer the reader to the original
account. It suffices here to say that it has given very fairly consistent
results at stations wide apart and that it promises to rival the invariable
pendulum.
CHAPTER III.
GRAVITATION.
CoNTKNTS.* — The Law of Gravitation — The Gravitation Constant and the Mean
Density of the Earth.
The full statement of Newton's Law of Gravitation is that any particle
of mass ]Mj attracts any other particle of mass M., distant d from it with a
force in the line joining them proportional to MjM.,/(Z-. The evidence for
the law may be briefly summed up as follows :
Starting with any single planet— say the earth — and referring its
position to a system, fixed relatively to the sun and the distant stars, direct
astronomical observation shows that it may be described with a close
approximation to the truth, as moving in an ellipse with the sun in one
focus, at such speed that the line from the centre of the sun to the centre
of the planet sweeps out equal areas in equal times. This implies, as
Newton showed, that the acceleration of the planet is towards the sun and
inversely as the square of its distance from that body.
Now, comparing the diflerent planet^^, observation shows that (length of
year)-/(niean distance)' is the same for each, and from this it follows that
the constant of acceleration is the same for all, or that at the unit distance
from the sun they would all have the same acceleration if the law holding
for each in its own orbit held for it at all distances.
So far this is mere time-geometry, or a description of position and rate
of change of position, and we might have other equally true, if less
convenient, modes of description referred to other standards, such as the
epicyclic geocentric mode of the ancients, or the practical mode in common
use in which the co-ordinates of a planet are measured with regard to some
observatory, its meridian, and horizon.
But if we regard the accelerations as indicating forces, the different
methods of description are no longer equivalent. We must select that
which gives a system of forces most consistent in itself and most in accord
with our terrestrial experience. Here the heliocentric method, with the
modification described hereafter, is immensely superior to any other, and,
adopting it, we must suppose that the accelerations of the planets indicate
forces towards the sun, and since the constant of acceleration is the same
for all, that the forces on equal masses are inversely as their distances
squared from the sun, whatever planets the masses belong to. In other
* This chapter is largely taken from TJie Mean Density of the Earth, and papers
comnuinicated to the Royal Institution and the Birmingham Natural History and
Vbilosophical Society, by J. H. Poynting.
GRAVITATION. £f)
words, the sun has no favourite among its attendants, but pulls on each
pound of each according to the same rule.
But the assumption that the accelerations indicate forces of the kind
we experience on the earth, carries with it the supposition of equality of
action and reaction, and so we conclude that each planet reacts on the sun
with a force equal and opposite to that exerted by the sun on the planet.
Hence, each acts with a force proportional to its own mass, and inversely
as the square of its distance away. If we suppose that there is nothing
special in the attraction of the sun beyond great magnitude corresponding
to great mass, we must conclude that the sun also acts with a force propor-
tional to its mass. But we have just shown that the force is proportional
to the mass acted on. Hence, we have the force on any planet proportional
to mass of sun x mass of planet /(distance apart)^.
Now, turning to any of the smaller systems consisting of a primary
and its satellites, the shape of orbit and the motion of the satellites agree
with the supposition that the primary is acting with a force according to
the inverse square law. It is important for our special problem to note
here that in the case of the earth we must include in the term " satellite "
any body at its surface which can be weighed or moved.
We are therefore led to conclude that the law is general, or that if we \
have any two bodies, of masses Mj and M^, at d distance apart, the force
on either is
GM,M,
d^~
where G is a constant — the constant of gravitation.
The acceleration of one of them, say M^, towards the other is ■ ^ t
d"
If this conclusion is accepted, we can at once determine the masses of
the various primaries in terms of that of the sun for —
acceleration of satellite towards primary = G-, '■ — " primary
distance of satellite'
and acceleration of primary towards sun = G- ^^^'^^ss ot sun
distance of primary'
By division G is eliminated, and we obtain the ratio of the masses in terms
of quantities which may be measured by observation.
As an illustration, let us make a rough determination of the mass of
the sun in terms of the mass of the earth.
We may take the acceleration of the moon to the earth as approxi-
mately wji^ y^ d^^^ where wm is the angular velocity of the moon and (/„ its
distance from the earth, and the acceleration of the latter to the sun as
WE-xc^ii where we is the angular velocity of the earth, and d^ its distance
from the sun. Let the mass of the sun be S and that of the earth be E.
, Acceleration of Moon _ w^" x cZ „ _ E x d^^
Acceleration of Earth we' x d^ S x d^ '
whence g = ^^ - l^\i^J$^^\'=mm
30 PROPERTIES OF MATTER.
A confirmation of the generality of the law is obtained from the
perturbations of the planets from the elliptic orbits which we have for
simplicity supposed them to describe.
These perturbations, in any one planet, can at least approximately be
analysed into separate disturbances, each due to one of its fellow planets,
acting with a foice inversely as the square of its distance away, and if we
assume this force proportional to the mass of the disturber we obtain
another measure for this mass in terms of that of the sun.
The concoidance of the two methods is as complete as we could
expect.
The determination of the masses of the different members of our system
in terms of that of the sun enables us to choose a still more satisfactory
origin for our system of reference than the centre of the sun — viz., the
centre of mass of the whole system. The change is small, but without it
we could not account for all the motions merely by a set of inverse square
forces in which action and reaction were equal and opposite.
We have for simplicity considered the sun and planets as without
appreciable dimensions as compared with their distances apart. But
measurement shows that they are all approximately spheres, and the
attraction on a sphere with density varying only with the distance from
the centre — i.e., consisting of homogeneous concentric shells, if itis considered
as the resultant of the attractions on the separate particles, all according
to the same inverse square law, is the same as that on the whole mass
collected at the centre of the sphere. Further, if the attraction is due, not
to the attracting body as a whole but to its separate parts, each acting, as
it were, independently and according to the same law, then an attracting
sphere acts as if it were all concentrated at its centre. Since the planets,
with a close approximation, behave as if they Avere merely concentrated
masses at their centres, and since the deviations from this behaviour, such
as the earth's precession, can all be accounted for by their departure from
sphericity, we have strong presumption that the attraction is really the
resultant of all the attractions, each element m^ of one body acting on each
element m^ of the other with force G')7i{nijd?.
Astronomical observation enables us, then, to compare the masses of
the various members of the solar system with each other, and, by taking
into account the sizes of the planets, to make a table of specific gravities,
choosing any one as the standard substance. Thus, if we take the earth
as standard, the mean specific gravity of the sun is about 0"2.5, that of
Mercury about 1'25, that of Venus and Mars about 0'9, and so on.
But this does not give us any idea of the specific gravity in terms of
known terrestrial substances or any idea of the masses in terms of the
terrestrial standards, the kilogramme or the pound. It is true that Newton,
with little more than the astronomical data at his command, made a
celebrated guess on the specific gravity of the earth in terms of water,
which runs thus in Motte's translation of the Principia (vol. ii. p. 230,
ed. 1729, Book III., Prop. 10) : " But that our globe of earth is of greater
density than it would be if the Avhole consisted of water only, I thus make
out. If the whole consisted of water only, whatever was of less density
than water, because of its less specific gravity, would emerge and float
above. And upon this account, if a globe of terrestrial matter, covered on all
sides with water, was less dense than water, it would emerge somewhere :
and the subsiding water falling back, would be gathered to the opposite
GRAVITATION. 31
side. And such is the condition of our earth, which, in great measure, is
covered with seas. The earth, if it was not for its greater density, would
emerge from the seas, and according to its degree of levity, would be raised
more or less above their surface, the water and the seas flowing backwarxls
to the opposite side. By tlie same argument, the spots of the sun which
float upon the lucid matter thereof, are lighter than that matter. And
however the Planets have been form'd while they were yet in fluid masses,
all the heavier matter subsided to the centre. Since, therefore, the common
matter of our earth on the surface thereof, is about twice as heavy as
water, and a little lower, in mines is found about three or four, or even five
times more heavy ; it is probable that the quantity of the whole matter of
the earth may be five or six times greater than if it consisted all of water,
especially since I have before shewed that the earth is about four timeg
more dense than Jupiter."
It is not a little I'emarkable that Newton hit upon the limits between
which the values found by subsequent researches have nearly all lain.
In order, then, to complete the expression of the law of gravitation we |
must connect the celestial with the terrestrial scale of densities. In fact, I
we must do for the masses of the solar system that which we do for their
distances in the determination of the solar parallax, though we cannot
proceed quite so directly in the former case as in the latter in connecting
the celestial and terrestrial measures. If we could measure the accele-
ration, say, of the moon, due to any terrestrial body of known shape
and density — if, for instance, we knew the form and extent of our
tidal-wave and its full lunar efiect— we could at once find the mass of
the earth in terms of that of the wave, or its density as compared with
sea-watei".
But at present this cannot be done with any approach to accuracy, and
the only method of solving the problem consists in finding the attraction
between two bodies on the earth of known masses a known distance apart,
and comparing this with the attraction of the earth on a known mass at
its surface instead of its attraction as a heavenly body. Since the law of
attraction is by observation the same at the surface of the earth and at a
distance, we can thus find the mass of the earth in terms of either of these
known masses.
To take an illustration from an experiment hereafter described, let us
suppose that a spherical mass of 20 kilos, is attracted by another spherical
mass of 150 kilos, when the centres are 30 cm. apart with a force equal to
the weight of ^ mgm. or s o o o^o o o o ^^ ^^^ weight of the 20 kilos, when
the latter is on the surface of the earth and 6 x 10^ cm. from its centre,
we have : (^ ^
Mass of Earth 1 50000 _., ^ ]
(6 X loy ' 30^ -^=¥ooooow --
whence mass of earth = 5 x 10-" grammes nearly.
The volume of the earth is about 9 x 10-'' c.c, whence the mean density
of the earth A is about 5'5.
Or, using the experiment to give the constant of attraction, and
expressing the masses in grammes, the weight of ^ mgm. or
AAAo- Gx 150000x20000
^30*
.^2
PROPERTIES OF MATTER.
Whence, if ^ = 98; G =
981 X -00025 x302_ 7
l5U0UUx20UU0 ~1U'
(nearly).
Due South of
SuiDinil onSlope
I .?
2"" StaHon
Due We^fof
First Station
A determination of G completes the expression of the law of
gravitation.
This example shows that the two problems, the determination of the
gravitation constant G and the determination of the mean density of the
earth A, are practically one, inasmuch as our knowledge of the dimensions
of the earth and the acceleration of gravity g at its surface at once
enable us to determine G if we know A, or to determine A if we
know G.
The Methods of Experiment.
These naturally fall into two classes. In the one class some natural
mass is selected, either a mountain or part of the earth's crust, and
its mass and form are more or less accurately
determined by surveys and mineralogical
examination. Its attraction on a plumb-
bob at one side, or on a pendulum above or
below it, is then compared with the attrac-
tion of the whole earth on the same body.
In the other, the laboratory class of
experiment, a smaller mass, such as may
be easily handled, is placed so as to attract
some small suspended body, and this attrac-
tion is measured. Knowing the attracting
and attracted masses, the attraction gives G.
Or, comparing the attraction with the attrac-
tion of the earth on the same body, we get A.
The Experiments of Boug-uer in
Peru. — The honour of making the first
experiments on the attraction of teri^estrial
masses is to be accorded to Bouguer. He
attempted both by the pendulum experi-
ments described in the last chapter, and by
plumb-line experiments, to prove the exist-
ence of the attraction of mountain masses in the Andes, when engaged in
the celebrated measurement of an arc of the meridian in Peru about the
year 1740. The pendulum experiments are sufliciently described in the
last chapter.
In his plumb-line experiments he attempted to estimate the sideway
attraction of Chimborazo, a mountain about 20,000 feet h'gh, on a plumb-
line placed at a point on its side. Fig. 8 will show the principle of the
method. Suppose that two stations are fixed, one on the side of the
mountain due south of the summit, and the other in the same latitude,
but some distance westward, away from the influence of the mountain.
Suppose that at the second station a star is observed to pass the meridian —
we will say, for simplicity, directly overhead, then a plumb-line hung
down will be exactly parallel to the observing telescope. At the first
station, if the mountain were away, it would also hang down parallel to
the telescope when dii-ectcd to the same star. But the mountain pulls the
plumb-line towards it, and changes the overhead point so that the star
J
Fig. 8. — Bouguer's Plumb-line Ex-
periment on the Attraction of
Cbimborazo.
GRAVITATION. 33
appears to northward instead of in the zenith. The method simply con-
sists in determining how much the star appears to be shifted to the north.
The angle of apparent shift is the ratio of the horizontal pull of the
mountain on the plumb- bob to the pull of the earth.
To carry out the experiment, Bouguer fixed the first station on the
south slope of Chimborazo, just above the perpetual snow-line, and the
second nearly on the same level, several miles to the westward. He
describes {Figure de la Terre, 7th section) how his expedition reached the
first station after a most toilsome journey of ten hours over rocks and
snow, and how, when they reached it, they had all the time to fight against
the snow, which threatened to bury theu^ tent. Nevertheless, they
succeeded in making the necessary observations, and a few days later they
were able to move on to the second station. Here they hoped for better
things, as they were now below the snow-line. But their dilficulties were
even gi^eater than before, as now they were exposed to the full force of the
wind, which filled their eyes with sand and was continually on the point
of blowing away their tent. The cold was intense, and so hindered the
working of their instruments that they had to apply fire to the levelling
screws before they could turn them. Still they made their observations,
and found that the plumb-line Avas drawn aside about 8 seconds. Had
Chimborazo been of the density of the whole earth, Bouguer calculated,
from the dimensions and distance of the mountain, that it w^ould have
drawn aside the vertical by about twelve times this, so that the earth
appeared to be twelve times as dense as the mountain, a result undoubtedly
veiy far wide of the truth. But it is little wonder that under
such circumstances the experiment failed to give a good result, and all
honour is due to Bouguer for the ingenuity and perseverance which enabled
him to obtain any result at all. At least he deserves the credit of first
showing that the attraction by mountain masses actually exists, and that
the earth, as a whole, is denser than the surface strata. As he remarks,
his experiments at any rate proved that the earth was not merely a hollow
shell, as some had till then held ; nor was it a globe full of water, as others
had maintained. He fully recognised that his experiments were mere
trials, and hoped that they would be repeated in Europe.
Thirty years later his hope was fulfilled. Maskelyne, then the
English Astronomer Royal, brought the subject before the Royal Society
in 1772, and obtained the appointment of a committee " to consider of a
proper hill whereon to try the experiment, and to prepare everything
necessary for carrying the design into execution." Cavendish, who was
himself to carry out an earth-weighing experiment some twenty-five years
later, was probably a member of the committee, and was certainly deeply
interested in the subject, for among his papers have been found calcula-
tions with regard to Skiddaw, one of several English hills at first con-
sidered. Ultimately, however, the committee decided in favour of
Schiehallion, a mountain near L. Rannoch, in Peithshire, 3547 feet high.
Here the astronomical part of the experiment was carried out in 1774,
and the survey of the district in that and the two following years. The
mountain has a short east and west ridge, and slopes down steeply on the
north and south, a shape very suitable for the purpose.
Maskelyne, who himself undertook the astronomical work, decided to
work in a way very like that followed by Bouguer on Chimborazo, but
modified in a manner suggested by him. Two stations were selected, one
C
34>
PROPERTIES OF MATTER.
z.l
rtn the south and the other on the north slope. A small observatory was
5rected first at the south station, and the angular distance of some staru
from the zenith, when they were due south, was most carefully measured.
The stars selected all passed nearly overhead, so that the angles measured
were very small. The instrument used was the zenith sector, a telescope
rotating about a horizontal east and west axis at the object-glass end, and
provided with a plumb-line hanging from the axis over a graduated scale at
the eyepiece end. This showed how far the telescope was from the vertical.
After about a month's woi'k at this station the observatory was moved
to the north station, and again the same stars were observed with the
zenith sector. Another month's work completed this part of the ex-
periment. Fig. 9 will show how the observations gave the attraction
due to the hill. Let us for the moment leave out of account the curvature
of the earth, and suppose it flat. Further, let us suppose that a star is
being observed which would be directly overhead if no mountain existed.
Then evidently at S. the plumb-line is
pulled to the north, and the zenith is
shifted to the south. The star therefore
appears slightly to the north. At N.
there is an opposite effect, for the moun-
tain pulls the plumb-line southwards,
and shifts the zenith to the north ; and
now the star appears slightly to the
south. The total shifting of the star is
double the deflection of the plumb-line
^uh'zci at either station due to the pull of the
mountain.
Fig. D.-Maskelyne's Plumb-line Ex- , ,^"*^ *^® Curvature of the earth also
periment on Schiehallion. deflects the verticals at N. and S., and
in the same way, so that the observed
shift of the star is partly due to the mountain and partly due to the
curvature of the eaith. A careful measure was made of the distance
between the two stations, and this gave the curvature deflection as about 43".
The observed deflection was about 55", so that the effect of the mountain,
the difference between these, was about 12",
The next thing was to find the form of the mountain. This was before
the days of the Ordnance Survey, so that a complete survey of the district
was needed. When this was complete, contour maps were made, giving
the volume and distance of every part of the mountain from each station.
Hutton was associated with Maskelyne in this part of the Avork, and he
carried out all the calculations based upon it, being much assisted by
valuable suggestions from Cavendish.
Now, had the mountain had the same density as the earth, it was
calculated from its shape and distance that it should have deflected the
plumb-lines towards each other through a total angle of 20-9", or 14 times
the observed amount. The earth, then, is 14 times as dense as the
mountain. From pieces of the rock of which the mountain is composed,
its density was estimated as 2i times that of Avater. The earth should
have, therefore, density 14 x 2| or 4J-. An estimate of the density of the
mountain, based on a survey made thirty years later, brought the result
up to 5. All subsequent work has shown that this number is not very
far from the truth.
GRAVITATION. S5
An exactly similar experiment was made eighty years later, on the
completion of the Ordnance Survey of the kingdom. Certain anomalies
in the direction of the vertical at Edinbuigh led Colonel James, the
director, to repeat the Schiehallion experiment, using Arthur's Seat as
the deflecting mountain. The value obtained for the mean density of the
earth was about 5 J.
Repetitions have also been made of the pendulum method, tried by
Boucuer in the Andes.
The first of these was by Carhni, in 1821. He observed the length of
a pendulum swinging seconds at the Hospice on Mont Cenis, about GOOO'
feet above sea-level, and so obtained the value of gravity there. The'
value due to mere elevation above the sea-level was easily calculated, but'
the observed value was greater than that calculated by about 1 in 5000.
In other words, the pull of the whole earth was 5000 times greater than
that of the mountain under the Hospice. Knowing approximately the
shape of the mountain, and estimating its density
from specimens of the rock, Carlini found the
density of the earth to be about 4^ times that of
water.
Another experiment of the same kind was
made by Mendenhall, in Japan, in 1880. Here
he determined the value of gravity on the
summit of Fujiyama, a mountain nearly 2| miles
high. He found it greater than the value
calculated fi'om the increased distance from the
earth's centre by about 1 in oOUO, as Carlini had
done on_ Mont Cenis. Fujiyama, though the ^^^Harto7?riSrtetr''*
higher, is more pointed and less dense than
Mont Cenis. Mendenhall estimated the mean density of the earth as
5-77.
Airy applied the pendulum to solve the problem in a somewhat dilTerent
way, using, instead of a mountain, the crust of the earth between the top
and the bottom of a mine. His first attempts were made in 1826, at the
Dolcoath copper mine, in Cornwall. Here he swung a pendulum first at
the surface and then at the bottom of the mine. At the point below we
may consider that the weight of the pendulum was due to the pull of the
part of the earth within the sphere with radius reaching from the earth's
centre to the point (Fig. 10). Knowing the value of gravity below, it
was easy to calculate what it would have been at the level of the surface
had no outer shell existed, and had the change in value depended merely
on the greater distence from the earth's centre. The observed value was
greater than this through the pull of the outer shell, and it was hoped
that the difference would be measured sufficiently accurately to show how
much greater is the mass of the earth than that of the crust. The first
attempt was brought to an end by a curious accident. As one of the
pendulums used was being raised up the shaft, the box containing it took
fire, the rope was burnt, and the pendulum fell to the bottom. Two years
later another attempt was made, but this was brought to an end by a
fall in the mine, which stopped the pump so that the lower station was
flooded.
Many years later, in 1854, the experiment was again undertaken by
Airy, this time in the Harton coal-pit, near Sunderland. The method waa
S6 PROPERTIES OF MATTER.
exactly the same, a pendulum being swung above and below the surface,
and the diminution in gravity above carefully determined. The experiment
was carried out with the gi-eatest care and in a most thorough way, two
pendulums being swung at the same time — one above and one below — the
two being interchanged from time to time. Several assistants were
occupied in taking the observations, which extended continuously night
and day for about three weeks. Now gravity at the surface was greater
than it would have been, had no outer shell existed of thickness equal to
the depth of the pit, by about 1 in 14,000, so that the pull of the earth
was about 14,000 times that of the shell. The density of the shell was
determined from specimens of the rocks, and Airy found the density of
the earth about 6|.
Some very interesting experiments have since been made in a similar
way by Von Sterneck in silver mines in Saxony and Bohemia. Using the
invariable pendulums described in the last chapter he obtained different
results with dilFerent depths of mines, the value of the mean density
increasing with the increasing thickness of the shell used. This shows
very evidently that there were sources of disturbance vitiating the method.
Von Sterneck found, on comparing his observations at the two mines, that
the increase in gravity on descending was much more nearly proportional
to the rise of temperature than to the depth of descent. This appears to
indicate that whatever disturbs the regularity of gravity disturbs also the
slope of temperature.
All the methods so far described use natural masses to compare the
earth with, and herein lies a fatal defect as regards exactness. We do not
know accurately the density of these masses and what is the condition of
the surrounding and underlying strata. We can really only form at the
best rough guesses. Indeed, the experiments might i-ather be turned the
other way about, and assuming the value of the mean density of the earth,
we might measui-e the mean density of the mountain or strata of which
the attraction is measured.
The Cavendish Experiment.
We turn now to a different class of experiment, in which the attracting
body is altogether on a smaller scale, so that it can be handled in the
laboratory. The smallness of the attraction is compensated for by the
accuracy with which we know the size and mass of the attracting body.
The idea of such an experiment is due to the Rev. John Michell, who
completed an apparatus for the purpose but did not live to experiment
with it.
Michell's plan consisted in suspending in a narrow wooden case a
horizontal rod G feet long, with a 2-incli sphere of lead hung at each end
by a short wire. The suspending wire for the rod was 40 inches long.
Outside the case were two lead spheres 8 inches in diameter. These were
to be brought up opposite the suspended splieres, one on one side, the
other on the other, so that their attractions on those spheres should con-
spire to turn the rod the same way round. Now moving each large sphere
on to the other side of the case so as to pull the suspended sphere with
equal force in the opposite direction, the rod should turn through twice the
angle which it would describe if the spheres were taken altogether away.
Hence half this angle would give the twist due to the attractions in one
GRAVITATION. 37
position alone. Knowing the torsion couple of the suspending wire for a
given angle of twist and the length of the rod, the attracting force would
be calculable. To find the torsion couple, Michell proposed to set the rod
vibrating. From its moment of inertia and time of vibration the couple
could be found.
Neglecting all corrections, the mathematics of the method may be
reduced to the following :
Let the two suspended balls have mass m each, the two attracting balls
mass M each. Let the rod have length 2a and with the suspended balls
moment of inertia I ; let d be the distance apart cf the centres of attracting
and attracted balls, and let 0 be the angle through which the attraction
twists the rod.
If /i is the toision couple per radian twist, and G the gravitation
constant, then
The time of vibration
whence, eliminating /i,
„ 2GM«irt.
27r Jllix,
47r^ie ^ 2GMma.
N" d'
Now we may obtain another equation containing G by expressing the
acceleration of gravity in terms of the dimensions and density of the
earth,
where r is the radius, 0 the circumference, and A the density of the
earth. Eliminating G between the last two equations and putting for
glir^ the length of the seconds pendulum L — a useful abbreviation — we
find
^ 3 L Mma N% '> ■
A = - X — X X — -'
4 C d' 10
where all the terms on the right hand are known or may be
measured.
On Michell's death the apparatus which he had collected for his
experiment came into the possession of Prof. Wollaston, who gave it to
Cavendish, Cavendish determined to carry out the experiment, with
certain modifications ; but he found it advisable to make the greater part
of the apparatus afresh, though closely following Michell's plan and
dimensions.
The actual work was done in the summer of 1797 and the following
spring tf 1798*
He selected for the experiment, according to Baily, an outhouse in his
garden at Clapham Common, and within this he appears to have constructed
an inner chamber to contain the apparatus, for he states that he "resolved
to place the apparatus in a room which should remain constantly shut, and
to observe the motion of the arm from without by means of a telescope,"
in order that inequalities of temperature and consequent air currents within
the case should be avoided.
* Experiments to determiue the density of the earth. Phi'. Irai.s., Ixxxviii,,
1798.
38
PROPERTIES OF MATTER.
The torsion rod h h (Fig. 11, reduced from the figure in Cavendish's
paper) was of deal, G feet long, strengthened by a silver wire tying the ends
to an upright m g in the middle. The two attracted balls x x were lead,
2 inches in diameter, and hung by short wires from the ends of the rod.
The torsion wire was o'd\ inches long, of silvered copper, and at first of
such cross section as to give a time of oscillation about 15m. This was
soon changed for one with a time of oscillation about 7m.
The position of the rod was determined by a fixed scale on ivory divided
to -^(jth. inch near the end of the arm, the arm itself carrying a vernier of
five divisions. This was lighted by a lamp outside the room, and was
viewed through a telescope passing through a hole in the wall.
The torsion case was supported on four levelling screws. The attracting
n:[-
Fig. 11. — Cavendish's Apparatus, h h, torsion rod hung by wire I /;; x x,
attracted balls hung from its ends; W VV, attracting masses movable
round axis P. T T, telescopes to view position of torsion rod.
masses, lead spheres 12 inches in diameter, WW, hung down from a cross
bar, being suspended by vertical copper rods. This bar could be rotated
by ropes passing outside the room round a pin fixed to the ceiling in the
continuation of the torsion axis.
The masses were stopped when |- inch from the case by pieces of wood
fastened to the wall of the building. When the masses were against the
stops their centres were 8'85 inches from the central line of the case.
The method of experiment was somewhat as follows : Tlie torsion rod
was never at rest, and the centi'e of swing was taken as the position in
which it would be if all disturbances could be eliminated. This centre of
swing was determined from three succeeding extremities of vibration when
the attracting masses WW were against the stops on one side. They were
then swung round so as to come against the stops on the other side of the
attracted masses, and the now centre of swing was observed. In a
particular experiment the dill'erence between the two centres was about
sij scale divisions. The time of vibration was observed from several suc-
cessive passages past the centre of swing, the value obtained in the saniQ
GRAVITATION. 39
experiment being about 427 sees., and the masses were then moved back
to their first position, giving a second value for the deflection.
In computing the results various coirections had to be introduced into
the equivalents of the simple formula; which have been given above.
Taking the attraction formula,
a correction had to be made, because the attracting masses were not quite
opposite those attracted, as the suspending bar was a little too short.
Then allowance was necessary for the attraction on the torsion rod, and a
negative correction had to be applied for the attraction on the more
distant ball. The copper suspending rods were also allowed for, and a
further correction was made for the change in attraction with change of
scale reading— i.e., for change of distance between attracting and attracted
masses. This correction was proportional to the deviation from the central
position, and may be regarded as an alteration of yn.
As to the case, it would evidently have no effect when the rod was
central, but it was necessary to examine its attraction when the rod was
deflected. Cavendish found that in no case did it exceed 1/1170 of the
attraction of the masses, and therefore neglected it.
Tui-ning now to the vibration formula,
this was correct when the masses were in the " midway" position — i.e., in
the line perpendicular to the torsion rod. But when they were in the
positive or negative position, the variation in their attraction, as the balls
approached or receded from them, made an appreciable alteration in the
value of the restoring couple, and thus virtually altered [i. The time had
therefore to be reduced by 2/185 of its observed value where S was the
deflection in scale divisions due to the change of the masses from midway
to near position.
But it is to be observed that, if the weights were moved from one near
position to the oti^er, and the time of vibration was taken in either
position, then the same correction having to be applied to fi in both
formulae, it might be omitted from both.
In all, Cavendish obtained twenty-nine results with a mean value of
D = 5-448 ±-033.
By a mistake in his addition of the results, pointed out by Baily, he
gave as the mean 5'48.
Repetitions by Reich, Baily and Cornu and Bailie.— His
experiment has since been repeated several times. Reich made two
experiments in Germany by Cavendish's method, obtaining in 1837 a
value 5'49, and about 1849 a value 5'58. In England it was repeated
by Baily about 1841 and 1842. Baily's experiment excited great attention
at the time, and the result obtained, 5'674, was long supposed to be very
near indeed to the truth. But certain discrepancies in the work gradually
impaired confidence in the final result, and in 1870 MM. Cornu and
Bailie, in France, undertook a repetition, with various improvements and
refinements. In planning out their own work they succeeded in detecting
40
PROPERTIES OF MATTER.
probably the chief source of error in Daily's work. They have as yet only
given an interim result of aboiit 5-5, and liave shown that Baily's work,
if properly interpreted, should bring out a not very difl'erent result. Their
final conclusion is still to be published.
Boys'S Cavendish Experiment. — Tn the Philosophical Transactions
for 18'J5 (vol. li^i), A. p. 1) is an account of a determination of the gravita-
tion constant carried out with the greatest care by Prof. Boys. He had
discovered a method of drawing exceedingly fine quaitz fibres and had
found them exceedingly
strong and true in their
elastic properties. They are
therefore pre-eminently ap-
plicable in torsion experi-
ments where small forces are
to be measured. Using a
quartz fibre as the torsion
wire in a Cavendish appara-
tus, he was able to reduce
the attracted Aveight and
the whole apparatus and yet
reduce the diameter of the
suspending fibre so far that
the sensitiveness was as great
as in earlier experiments.
At the same time the small-
ness of the apparatus allowed
it to be kept at a much more
uniform temperature, and
the disturbances due to con-
vection air currents were
much lessened. These dis-
turbances had much troubled
the earlier workers. In Fig.
12 is a diagrammatic repre-
sentation of the apparatus.
The attracted masses mm
were of gold, one pair 0-2
inch, another pair 0'25 inch
in diameter. The torsion
rod N was 0-9 inch
and
Fig. 12. — Diagrammatic Ktpreseritatioii of a Section of
Boys's Apparatus.
long
was
was itself a mu-ror in
which the reflection of a scale distant about 23 feet, and divided to 50ths
of fin inch, was viewed. The quartz fibre was 17 inches long.
The attracting masses MM were lead balls 4| inches in diameter. Had
the masses all been on one level, as in the original arrangement, with such
a short torsion rod the attracting masses wotild have attiacted both gold
balls nearly equally. To avoid this. Boys had one attracting and one
attracted mass at one level and the other two at a level six inches below.
The balls mm were hung from the torsion rod by quartz fibres inside a
tube about ] h inches diameter. The atti'actinjr masses MM were hung
from the revolving lid of a concentric tubular case about 10 inches in
fliametci'. These masses were ariangod in tie position in which they
GRAVITATION. 41
exerted the maximum couple on the gold balls first in one direction and
then in the opposite. The deflection varied from o51 to u77 divisions,
according to the balls used and the times of vibration from 188 to 242
seconds. The apparatus was moat exactly constructed and measured, and
the results were very concordant.
The final value, probably the best yet obtained, was :
G = G-G57G X lO^^jwhence A=_5j)270
Braun'S Experiment {Denhschrift. der Math. Nat. Classe der Kais.
Ahad. Wien. 1896. Bd. Ixiv.). — In 189G Dr. Braun published an account
of an experiment carried out by him. He used the torsion-rod method,
and though his apparatus was considerably larger than that of Boys, it
was still much smaller than that of Cavendish, Reich or Baily. The
rod was about 24 cm. long and was suspended from a tripod by a brass
torsion wire nearly one metre long and 0*055 mm. in diameter. The
whole torsion arrangement was under a glass receiver, about a metre high
and 30 cm. in diameter, resting on a flat glass plate. The receiver could be
exhausted and in the later experiments the pressure was about 4 mm. of
mercury and the disturbances due to air cuirents were very greatly
reduced. The attracted masses at the end of the rod were gilded brass
spheres each weighing about 54 gms. Round the xipper part of the
receiver, and outside it, was a graduated metal ring which could be
revolved about the axes of the toi-sion wire ; from this were suspended,
about 42 cm. apart, the two attracting masses. Two pairs were used, one
a pair of bi-ass spheres about five kgms. each, the other a pair of iron
spheres filled with mercury and weighing about nine kgms. each.
Special arrangements had to be used to determine the position of the
rod by means of a mirror fixed on its centre, the beam being reflected
down through the bottom of the plate. The time of vibration was about
1275 sees. The result obtained was very near to that of Boys, viz. :
G = G-G578GxlO-8; A = 5-52725
A result very nearly the same has recently been obtained by von
Eotvos {Wied. Ann. 59, 189G, p. 354), but he has not yet completed the
work.
Wilsing's Experiment. — About 1886, Dr. Wilsing, of Potsdam,
devised a modified form of Cavendish's experiment, in which a sort of
double pendulum is used — i.e., one with a ball below and another at a
nearly equal distance above the suspension. The pendulum is then in a
very sensitive state, and a very small horizontal force pulls it through a
large angle.
It is then just like a toi'sion balance, but with a vertical instead of a
horizontal rod. If weights are brought up, one to pull the upper ball to
one side and the other to pull the lower ball to the other side, the
pendulum twists round slightly. From the observed twist and the time
of swing the attraction can be measured and compared with the pull of
the earth. Wilsing found that the earth had a mean density of 5'579.
Experiments with tlie Common Balance.
Von Jolly's Experiment. — In 1878 and in 1881 Professor von Jolly
described a method which he had devised. He had a balance fixed at the
42
PROPERTIES OF MATTER.
top of a tower in Munich, and from the scale-pans hung wires supporting
two other scale-pans at the bottom of the tower (21 metres below).
Imagine that two weights are balanced against each other at the top of
the tower. If one is now brought down and put in the lower scale-pan on
the same side it is nearer the centre of the earth, and, therefore, heavier.
Von Jolly found a gain of about 32 milligrammes in 5 kilogrammes. He now
built up a large lead sphere under the lower pan, a yard in diameter, so that
its attraction was added to that of the earth. The gain on transferring
the weight from the upper to the lower pan now came out to about half a
milligramme more, so that the attraction of the sphere was this half milli-
gramme. The earth's attraction was about 10,000,000 times that of the
sphere, and its density was calculated to be 5"G*J.
Fig. 13.— EicharB and Krigar-Merzel'B Experiment.
Experiment of Richarz and Krig-ar-Menzel.— An experiment
very much like that of Yon Jolly in piinciple has been carried out by
Drs. Richarz and Krigar Menzel at Spandau, near Berlin (Abhand. der
K'onigl. Preuss Akad. Berlin, 1898), A balance with a beam 23 cm.
long was supported at a height above the floor, and from each end
were suspended two pans, one near the beam the other near the floor,
more than two metres lower. Fig. 13. In principle the method was as
follows : Spherical gilded or platinised copper weights wore used, and to
begin with these were placed, say, one in the right-hand top pan, the other
in the left-hand bottom pan. Suppcse that in this position they exactly
balanced. The weights were then moved, the right-hand one into the
right lower pan, when it gained weight through the increase of gravity
with a descent of over two metres ; the left-hand one into the left upper
pnn, when it lost weight thi-ough the ascent of the same amount. The
result after corrections was that the right-hand pan appeared heavier by
1"24:53 mgm., half this being due to the change in position of a single
kilogramme.
GRAVITATION. 43
A lead parallelepiped was now built up of separate blocks, between the
upper and lower pans, 2 metres high and 2'1 metres square, horizontally,
with passages for the wires suspending the lower pans. The weighing
of the kilogrammes was now repeated, but the attraction of the lead,
which was reversed when a weight was moved froai bottom to top, was
more than enough to make up for the decrease in gravity, and the right-
hand now appeared lighter on going through the same operation by
0*1211 mgm. ; whence the attraction of the lead alone made a dilFei'ence
of 1-36G4 mgm. This is four times the attraction of the lead on a single
kilogramme. Knowing thus the pull of a block of lead of known form and
density on the kilogramme at a known distance, and knowing too the pull
of the earth on the same kilogramme, viz., 10" mgm., the mean density of
the earth could be found.
The final result was :
G = 6-G85xl0-»
A = 5-505
Poynting"'S Experiment. — The method of using the balance in this
experiment will be gathered from Fig. 14. A B are two lead weights
about 50 lb. each, hanging down from the ends of a very large and strong
balance inside a protecting wood case. M is a large lead sphere, weighing
about 350 lb., on a turn-table, so that it can move round from under A till
it comes under B. The distance between the centres of M and A or M
and B is about one foot. When under A, M pulls A, and so increases its
weight. When moved so as to come under B the increase is taken from
A and put on to B. The balance is free to move all the time, so that it
tilts over to the B side an amount due to double the attraction of M
on either, m was a balance weight half the mass of M, but at double the
distance. Before this was used it was found that the movement of M
tilted the floor, and the balance, which was a very sensitive level, was
afiected by the tilt.
To observe the deflection due to the alteration in weight, a mirror was
connected with the balance pointer by the " double suspension " method,
due to Lord Kelvin, and shown in Fig. 15.
With the suspension the mirror turned through an angle 150 times as
great as that turned through by the balance beam. In the x-oom above
was a telescope, which viewed the reflection of a scale in the mirror, and
as the mirror turned round the scale moved across the field of view. The
tilt observed meant that the beam turned through rather more than 1",
and that the weight moved nearer to the mass by about y ^Vo ^^ ^^ inch.
The weight in milligrammes producing this tilt had to be found. This was
done virtually (though not exactly in detail) by moving a centigiamme
rider about 1 inch along the beam, which was equivalent to adding to one
side a weight of about ^0 milligramme. The tilt due to the transfer was
observed, and was found to be very nearly the same as that due to the
attraction, so that the effect of moving M round from A to B was
equiv^alent to increasing B by -^o milligramme, or ^^oooovQ ^^ ^^^ previous
weight. The pull on either is half this. In other words, the earth pulled
either about 100,000,000 times as much as the mass M, and the earth,
which is 20,000,000 times as far away, would at the same distance have
exerted 400,000,000,000,000 times 100,000,000 times the pull, and is,
therefore, so many times heavier. Thus we find that the earth weighs
4>4
PROPERTIES OF MATTER.
about 1-25 X 10-^ lb. In obtaining the attraction of M on A or B, the
attraction on the beam had to be eliminated. This was done by moving
the masses A B into the positions A' B' one foot higher, and finding
Fig. 14. — Poynting's Experimect. A U, weights, each about 50 lb., hanging from
the two anas of balance. M, attracting mass on turn-table, movable so as to
come under either A or B. m, balancing maos. A' B', second positions for A
and B. In this position the attraction of M on the beam and suspending wirps
is the same as before, so that the difference of attr.iction on A and B in tlie
two positions is due to the difference in distance of A and B only, and thus the
attraction on the beam, &c., is eliminated.
the attraction in this position. The difference was due to the chinge
in A and B alone, for the attraction on the beam remained the Siime
throughout.
The final result was —
G = G-G984xlO«
A = 5-i934
GRAVITATION.
45
Experiments on the Qualities of Gravitation.
The Rang-e of Gravitation. — The first question which arises is,
whether the law of gravitation holds down to the minutest masses and
distances which we can deal with. All our observations and experiments
go to show that it holds throughout the long range fiom interplanetary
Microscope stage
^radu^
^gUllUa.
I Mirror
J
Varies u^crkon^
in dcishpot
Fig. 15 — Double Suspension Mirror (half sizeX
distances down to the distances between the attracting bodies in the
laboratory experiments described above.
The first step in the descent from celestial spaces is justified by the fact
that the acceleration of gravity at the earth's surface agrees with its value
on the moon, as attracted by the earth. The further step downward
appears to be justified by the fair agreement of the results obtained by the
various forms of Cavendish, balance, and pendulum experiments on the
mean density — expeinments which have been conducted at distances varying
from feet down to inches. Where the law ceases to hold is yet a matter for
experiment to determine. When bodies come into what we term " contact,"
the adhesion may possibly still be due to gravitation, according to the inverse
square law, though the varying nature of the adhesion in different cases
seems to point to a change in the law at such minute distancesT
4-6 PROPERTIES OF MATTER.
Gravitation not Selective.— it might be possible that some matter
is attracted more tlum in proponion to its mass and some less. The agree-
ment of astronomical observations with deductions from the general law is
not perfectly decisive as to this possibility, for there might be such a
mixture of dillerent kinds of matter in all the planets that the general
average attraction was in accordance with the law though Hot the attraction
on each individual kind. A supposition somewhat of this description is
required in an explanation which has been given of the formation of
comets' tails, some matter in the comet being supposed to be acted on by
the sun, not by the ordinary law but by a repulsion. This explanation is,
however, now generally abandoned, an electrical origin of the tails being
regarded as more probable.
But, with regard to ordinary terrestrial matterj l^ewton's hollow
pendulum experiments {Principia, Book III., Prop. C) repeated with more
detail and precision by Bessel {Versuche iiber die Kraft, niit welcher die
Erde Kijrper von verschiedenerBeschaffenheit anzeiht, Abhand. der Berl.
Ak. 1830, p. 41; or Memoires relatifs d, la Physique, tome v. pp. 71-
133) prove that the earth as a whole is not selective. Still, the results
Fig. 16. — raramagnetic Sphere placed Fig. 17. — Diamagnetic Sphere placed
in a previously Straight Field. in a previously Straight Field.
might just conceivably be due to an average of equal excesses and defects.
But again we may quote the various mean density experiments, and especially
those made by Baily, in which a number of different attracting aod attracted
substances have been used with nearly the same results.
Gravitation not Affected by the Medium. — When we compare
gravitation with other known forces (and those which have been most
closely studied are electric and magnetic forces) we are at once led to
inquire wdiether the lines of gravitative fo';ce are always straight lines
radiating fi-om or to the mass round which they centre, or whether, like
electric and magnetic lines of force, they have a preference for some media
and a distaste for others. We knov/, for example, that if a magnetic
sphere of iron, cobalt or manganese is placed in a previously straight field,
its permeability is greater than the air it replaces, and the lines of force
crowd into it, as in Fig. 16. The magnetic action is then stronger in the
presence of the sphere near the ends of a diameter parallel to the original
course of the lines of force, a-ad the lines are deflected. If the sjihere be
diamagnetic, of water, copper, or bismuth, the permeability being less
than that of air, there is p,a opposite effect, as in Fig. 17, and the field is
weakened at the ends of a diameter parallel to the lines of force, and again
the lines aie deflected. Similarly, a dielectric body placed in an electric
field gatheis in the lines of force, and makes the field where the lines enter
and leave stronger than t was before.
\
GRAVITATION. 47
If we enclose a magnet in a hollow box of soft iron placed in a
magnetic field, the lines of force are gathered into the iron and largely
cleared away from the inside cavity, so that the magnet is screened from
external action.
Astronomical observations are not conclusive against any such effect of
the medium on gravitation, for the medium intervening between the sun
and planets approaches a vacuum,where so far we have no evidence for
variation in quality, even for electric and magnetic induction. In the case
of the earth, too, its spherical form might render observation inconclusive,
for just as a sphere composed of concentric dielectric shells, each with its
surface uniformly electrified, would have the same external field in air,
whatever the dielectric constant, if the quantity of electrification within
were the same, so the earth might have the same field in air whatever the
varying quahty of the underlying strata as regards the transmission of the
action across them, if they were only suitably arranged.
But common experience ^__,,^ b
might lead us at once to ^^^^^."''^'''''^
say that there is no very --"l5t^^^'^'^--i>^^^^''''
considerable efiect of the .-^^^•^^"■^^^^TT^^^^^-^^^^^^ — -j^^^^^^^^^^^
kind with gravitation. The .,^<:^^^^^^^^^ir^^^c^--'" ' '^^^^^^^^^^^'^
evidence of ordinary weigh- ^^^^^^^'. ^^" /Z —
ings may, perhaps, be re- ^ — ■
jected, inasmuch as both ^"'*°''^^^^^=^^n~---^^C:/"-----^^
sides will be equally af- """^^^^^>^>.^ '^
fected as the balance is ^'''*"^~~-^--~__
commonly used. But a -c, m i-a i. « • i •,.• « ii„
•^ Fig. 18. — Effect of interposition of more permeable
spring balance should show Medium in radiating Field of Force.
if there is any large effect
when used in different positions above different media, or in different
enclosures. And the ordinary balance is used in certain experiments in
which one weight is suspended beneath the balance case, and surrounded,
perhaps, by a metal case, or, perhaps, by a water-bath. Yet no appreciable
variation of weight on that account has yet been noted. Nor does the
direction of the vertical change rapidly from place to place, as it would
with varying permeability of the ground below. But perhaps the agreement
of pendulum results, whatever the block on which the pendulum is placed,
and whatever the case in which it is contained, gives the best evidence
that there is no great gathering in, or opening out of the lines of the
earth's force by different media.
Still, a direct experiment on the attraction between two masses with
different media interposed was well worthy of trial, and such an experiment
has been carried out by Messrs. Austin and Thwing.* The effect to be
looked for will be understood from Fig. 18. If a medium more permeable
to gravitation is interposed between two bodies, the lines of force will
move into it from each side, and the gravitative pull on a body, near the
interposed medium on the side away from the attracting body, will be
increased.
The apparatus they used was a modified kind of Boys's apparatus
(Fig. 19). Two small gold masses in the form of short vertical wires, each
•4 gm. in weight, were arranged at different levels at the ends virtually of
a torsion rod 8 mm. long. They are represented in the figure by the two
* Physical Review, v. 1897, p. 294.
48
PROPI'.RTIES OF MATTER.
thickenings on the suspending fibre. The attracting masses MjM, were lead,
each about 1 kgm. These were first in the positions shown by black lines in
the figure, and were then moved into the positions shown by dotted lines.
The attraction was measured first when merely the air and the case of the
instrument intervened, and then when various slabs, each 3 cm. thick, 10
cm. wide and 29 cm. high, were interposed. With screens of lead, zinc,
mercury, water, alcohol or glycerine, the change in attraction was at the
most about 1 in 500, and this did not exceed the errors of experiment.
That is, they found no evidence of a change in pull with change of medium.
If such change exists, it is not of the order of the change of electric pull
with change of medium,
but something far smaller.
It still remains just pos-
sible, however, that there
are variations of gravita-
tional permeability compar-
able with the vaiiations of
magnetic pei-meability in
media such as water and
alcohol.
Gravitation not Di-
rective. — Yet another
kind of eflfect might be sus-
pected. In most crystalline
substances the physical pro-
perties are different along
different directions in a
crystal. They expand dif-
ferently, they conduct heat
differently, and they trans-
mit light at different speeds
in different directions. We
might then imagine that
the lines of gravitative force
spread out from, say, a crys-
tal sphere unequally in dif-
ferent directions. Some
years ago Dr. Mackenzie* made an experiment in America, in which he
sought for direct evidence of such unequal distribution of the lines of
force. He used a form of apparatus like that of Professor Boys (Fig. 12),
the attracting masses being calc spar spheres about 2 inches in diameter.
The attracted masses in one experiment were small lead spheres about
^ gm. each, and he measured the attraction between the crystals and the
lead when the axes of the crystals were set in various positions. But the
variation in the attraction was merely of the order of error of experiment.
In another experiment the attracted masses were small calc spar crystal
cylinders weighing a little more than I gm- each. But again there was no
evidence of variation in the attraction with variation of axial direction.
Practically the same problem was attacked in a different way by
Poynting and Gray.t They tried to find whether a quartz crystal sphere
* Physical Review, ii. 1895, p. 321.
t PhU. Trans., 192, 1899, A. p. 245.
•■'o""-.
1 S .^-,1
1 .' H-- I
\ \
/ •' (
' m' •■O-.
[yb/ \
\
•.. (
) /
"\
(
■
y
■\
/
V
\
1 A^
! /'/' :
''\"v
11 1
1
3
c—
1
:::■ -
-
^
. 1
Fig. 19. — Experiment on Gravitative Permeability
(Austin and Thwing).
GRAVITATION. 49
had any directive action on another quartz crystal sphere close to it, whether
they tended to set with their axes parallel or crossed.
It may easily be seen that this is the same problem by considering
what must happen if there is any diflerence in the attraction between two
such spheres when their axes are parallel and when they are crossed.
Suppose, for example, that the attraction is always greater when their axes
are parallel, and this seems a reasonable supposition, inasmuch as in
straightforward crystallisation successive parts of the crystal are added to the
existing crystal, all with their axes parallel. Begin, then, with two quartz
crystal spheres near each other with their axes in the same plane, but
perpendicular to each other. Remove one to a very great distance, doing
work against their mutual attractions. Then, when it is quite out of range of
appreciable action, turn it round till its axis is parallel to that of the lixed
crystal. This absorbs no work if done slowly. Then let it return. The
force on the return journey at every point is greater than the force on the
outgoing journey, and more work will be got out than was put in. When
the sphere is in its first position, turn it round till the axes are again at
right angles. Then work must be done on turning it through this right
angle to supply the diflerence between the outgoing and incoming works.
For if no work were done in the turning, we could go through cycle after
cycle, always getting a balance of energy over, and this would appear to
imply either a cooling of the crystals or a diminution in their weight, neither
supposition being admissible. We are led then to say that if the attraction
with parallel axes exceeds that with crossed axes, there must be a directive
action resisting the turn from the crossed to the parallel positions. And
conversely, a directive action implies axial variation in gravitation.
The straightforward mode of testing the existence of this directive
action would consist in hanging up one sphere by a wire or thread, and
turning the other round into various positions, and observing whether the
hanging sphere tended to twist out of position. But the action, if it exists,
is so minute, and the disturbances due to air currents are so great, that it
would be extremely difiicult to observe its efiect directly. But the prin-
ciple of forced oscillations may be used to magnify the action by turning
one sphere round and round at a constant rate, so that the couple would
act first in one direction and then in the other alternately, and so set the
hanging sphere vibrating to and fro. The nearer the complete time of
vibration of the applied couple to the natural time of vibration of the
hanging sphere, the greater would be the vibration set up. This is well
illustrated by moving the point of suspension of a pendulum to and fro in
gradually decreasing periods, when the swing gets longer and longer till
the period is that of the pendulum, and then decreases again. Or by the
experiment of varying the length of a jar resounding to a given fork, when
the sound suddenly swells out as the length becomes that which would
naturally give the same note as the fork. Now, in looking for the couple
between the crystals, there are two possible cases. The most likely is that
in which the couple acts in one way while the turning sphere is moving
from parallel to crossed, and in the opposite way during the next quarter ■
turn from crossed to parallel. That is, the couple vanishes four times
during the revolution, and this we may term a quadrantal couple. But it
is just possible that a quartz crystal has two ends like a magnet, and that
like poles tend to like directions. Then the couple will vanish only twice
.11 a revolution, and may be termed a semicircular couple. Both were
D
50 PROPERTIES OF MATTER.
looked for, but it is enough now to consider the possibility of the quadrantal
couple only.
The mode of working will be seen from Fig. 20. The hanging sphere,
•9 cm. in diameter and 1 gm. in weight, was placed in a light aluminium
wire cage with a mirror on it, and suspended by a long quartz fibre in a
brass case with a window in it opi)Osite the mirror, and surrounded by a
double-walled tinfoiled wood case. The position of the sphere was read in
^f To Accujni
tneUned Mirror [p
'Gf (J
?????^?^
•d*
"^^^
\i
w5
IE
(3
Fig. '20. — Experimeut on directive Action of one Quartz Crystal on another.
the usual way by scale and telescope. The time of swing of this little
sphere was 120 seconds.
A larger quartz sphere, 6 "6 cm. diameter and weighing 400 gms., was
fixed at the lower end of an axis which could be turned at any desired rate
by a regulated motor. The centres of the spheres were on the same level
and 5-9 cm. apart. On the top of the axis was a wheel with 20 equidistant
marks on its rim, one passing a fixed point every 11*5 seconds.
It might be expected that the couple, if it existed, would have the
greatest efiect if its period exactly coincided witli the 1 20-second period of
the hanging sphere — i.e., if the larger sphere revolved in 210 seconds. But
in the conditions of the experiment the vibrations of the small sphere were
very much damped, and the forced oscillations did not mount up as they
would in a freer swing. The disturbances, which were mostly of au im-
GRAVITATION.
51
pulsive kinfl, continiinlly set the hanging sphere into large vibration, and
these might easily be taken as due to the revolving sphere. In fact,
looking for the couple with exactly coincident periods would be something
PkrwdL VZ5
Fia. 21. — Upper Curve a regular Vibration.
Disturbance dying away.
Lower Curve a
Sfj
like trying to find if a fork set the air in a resonating jar vibrating when
a brass band was playing all round it. It was necessary to make the
couple period, then, a little difi'erent from the natural 120-second period,
and accordingly the large sphere was revolved once in 230 seconds, when
the supposed quadrantal couple would have a
period of 115 seconds.
Figs. 21 and 22 may help to show how
this tended to eliminate the disturbances.
Let the ordinates of the curves in Fig. 21
represent vibrations set out to a horizontal
time scale. The upper curve is a regular
vibration of range ± 3, the lower a disturbance
beginning with range ±1(*. The first has
period 1, the second period l"2r). Now, cutting
the curves into lengths equal to the period of
the shorter time of vibration, and arranging
the lengths one under the other, as in Fig. 22,
it will be seen that the maxima and the
minima of the regular vibration always fall at
the same points, so that, taking 7 periods, and
adding up the ordinates, we get 7 times the
range, viz., ±21. But in the disturbance the
maxima and minima fall at different points,
and even with 7 periods only the range is
from + 16 to - 13, or less than the range due
to the addition of the much smaller regular
vibration.
In the experiment the couple, if it existed,
would very soon establish its vibration, which would always be there, and
would go through all its values in 115 seconds. An observer, watching
7^^
Fio. 22.— Results of Superposi.
tion of Lengtbj of Curves iu
Fig. 21 equal to tlie Period of
the regular one.
bi PROPERTIES OF MATTER.
the wheel at the top of the revolving axis, gave the time signals every 1 1 -5
seconds, regulating the speed if necessary, and an observer at the telescope
gave the scale reading at every signal, that is, 10 times during the period.
The values were arranged in 10 columns, each horizontal line giving the
readings of a period. The experiment was carried on for about 2^ hours
at a time, covering, say, 80 periods. On adding up the columns, the
maxima and minima of the couple efiect would always fall in the same two
columns, and so the addition would give 80 times the swing, while the
maxima and minima of the natural swings due to disturbances would fall
in different columns, and so, in the long run, neutralise each other. The
results of different days' work might, of course, be added together.
There always was a small outstanding effect such as would be produced
by SI quadrantal couple, but its effect was not always in the same columns,
and the net result of observations over about 350 periods was that there was
no 115 -second vibration of more than 1 second of arc, while the disturbances
were sometimes 50 times as great. The semicircular couple required the
turning sphere to revolve in 115 seconds. Here, want of symmetry in the
apparatus would come in with the same effect as the couple sought, and
the outstanding result was, accordingly, a little larger. But in neither case
could the experiments be taken as showing a real couple. They only showed
that, if it existed, it was incapable of producing an effect greater than that
observed. Perhaps the best way to put the result of the work is this : Imagine
the small sphere set with its axis at 45° to that of the other. Then the
couple is not greater than one which would take 5J hours to turn it
through that 45° to the parallel position, and it would oscillate about that
position in not less than 21 hours.
The semicircular couple is not greater than one which would turn from
crossed to parallel position in 4| hours, and it would oscillate about that
position in not less than 17 hours. Or, if the gravitation is less in the
crossed than in the parallel position, and in a constant ratio, the difference
is less than 1 in 16,000 in the one case and less than 1 in 2800 in the other.
We may compare with these numbers the difference of rate of travel
of yellow light through a quartz crystal along the axis and perpendicular
to it. That difference is of quite another order, being about 1 in 170.
Other possible Qualities of Gravitation. — Weight might con-
ceivably change with temperature, but experiments * show that if there is
any change it is probably less than 1 in 10^' of the weight per 1° C.
It is possible that weight might change when the bodies weighed enter
into chemical combination. Many experiments have been made to detect
such a change, the most extensive and exact by Landolt.t At first it
appeared as if in sdme cases a diminution of weight occurred on combina-
tion, but ultimately the effect was traced to an expansion of the containing
vessel through the heat developed. The vessel did not return at once to
its original volume on cooling and so there was a slight increase in the
buoyancy of the air in the weighing after combination. The experiments
show that the change, if it exists, is too small to measure.
No research yet made has succeeded in showing that gravitation is
related to anything but the masses of the attracting and the attracted
bodies and their distance apart. It appears to have no relation to physical
or chemical conditions of the acting masses or to the intervening medium.
* Poynting &Phillips,P.;?.,S'.,A 76, 1905, p. 445; Southern8,P.ii.5.,A78, 1906, p. 392.
f Landolt, Preuss. Ak. Wiss. Berlin, Sitz. Ber., viii. 1906, p. 266, and xvi. 1908,
March 19. References to other work are given in the first paper.
CHAPTER IV.
ELASTICITY.
Contents. — Limits of Elasticity — Elastic after effect — Viscosity of Metals and
Elastic Fatigue — Anomalous Effects of first Loading a Wire — Breakir/g Stress.
In this chapter we shall consider changes in the conformation of solid
bodies and the connection between these changes and the forces which
produce them.
Many of the points with which we shall have to deal are well
illustrated by the simple case of a vertical metal wire the upper end of
which is fixed while the lower end carries a scale-pan. If we measure
the increments of elongation of the wire when different weights are
placed in the scale-pan and plot our results as a curve in which the
abscissae are the elongations of the wire — i.e., the extension of the wire
divided by its unstretched length, and the ordinates the stretching weight
(inclusive of the weight of the scale-pan) divided by the area of cross
section of the unstretched wire, we obtain results similar to those shown
in Fig. 23 (from A History of the Theory of Elasticity and of the Strength
of Materials), which represents the results of experiments made by Professor
Kennedy on a bar of soft steel.
The first part of the curve — when the stretching force per unit area is
less than a certain value, is a straight line — i.e., up to a certain point the
elongationjs proportional to the load per unitj-rea of cross section,* and
up to this point we find that whenjwe remoWthe weight from the scale-
pan jthe stretched wire shortens u ntil its length is the same as it was
before the weights were put ^on_ (the elongations in this stage are so
small thaton the scale of Fig. 23 this part of the curve is hardly distinguish-
able from the axis AB). When, however, we get beyond a certain
point B on the curve — i.e., when the stretching foi-ce per unit area is
greater than the value represented by AB, the curve becomes bent, and
we find on removing the weights that the wire does not return to its
original length , but is permanently lengthened, and is Bai3~to^ have
axx^mredrpermahentjet.
The range of elongations over which the wire, when unloaded, recovers
its original length, is called the range_of perfect elasticity; when we
go beyond this range we are said to exceed the elastic limit.
* This seems to be only approximately true for certain kinds of iron. {A Hiitory
of the Theory of Maatioity and of the Strength of Materials. Todhunter and Tcarsou,
Vol. i. p. 893.
54
PROPERTIES OF MATTER
After passing the point represented by B a stage is readied where the
extension becomes very large. Tlie scale-pan runs rapidly down and the
wire looks as if it wei-e about to break. By far_the greater part of this
extension is _permanent, and the wire, after passing the state represented
by C, is not able to sustain as great a pull as before without sufiering
further elongation ; this is shown by the bending back of the curve. The
place C where this great extension begins is called the yield-point ; it
seems to be always fm^ther along the curve than the elastic limit B.
S
\A.
H ExZcfhsioiv.
Fig. 23.— Elongation of a Sti etched Wire.
The part of the incrcnient of elongation which disappears on the
removal of the stretchiui; weiirht, between the elastic limit and the yield-
point, is proportional to the stretching;_weight, and the ratio of this
ELASTICITY. 55
movement to tlie stretching weight per unit area is, according to the
experiments of Professor Kennedy, the same as that within tlio limits of
perfect elasticity {see Todhunter and Pearson's History of Elasticity,
p. 889).
After passing the yield-point the elongation increaees very rapidly
with the load, and at this stage the wire is plastic, the elongation
depending upon the time the stretching force acts. The extension rapidly
increases and the area rapidly contracts until the breaking- point E is
reached. The apparent maximum for the load per unit area shown in
Fig. 23 is due to the contraction of the area, so that the pull per unit area
of the stretched wire is no longer represented even approximately by the
ordinates. About the point D the wire begins to thin down or flow
locally, so that its cross section is no longer uniform, some parts being now
smaller than the rest.
The portion GHG' of the curve represents the effect of unloading
and reloading at a point G past the yield point. We see, from the shape
of this portion of the curve, that the limit of perfect elasticity for this
permanently stretched wire has been extended beyond the yield-point of
the wire before it was permanently stretched. The range between the
limit of perfect elasticity and the breaking-point is very different for
different substances ; for ductile substances, such as lead, it is considerable,
while for b}'ittle ones, such as glass, it is evanescent.
We are thus from our study of the loaded wire led to divide the
phenomena shown by substances acted upon by forces into two divisions —
qne^ divisiQn_in which the solid recovers its original form after the
removal of the forces which deformed it, the other division in which a
permanenJL-clLange is produced by the application of the force! Even,
within the limits of perfect elasticity different bodies show distinct
differences in their behaviour. Some recover their form immediately
after the removal of the force, while others, though they recover it
ultimately, take considerable time to do so. Thus a thread of quartz fibre
will recover its shape immediately after the removal of the tensional
and torsional forces acting upon it, while a glass fibre may, if the forced
have been applied for a considerable time, be several hours before it
regains its original condition. This delay in recovering the original
condition of the substance is called the elastic after-effect ; it may be
conveniently studied in the case of the torsion of glass fibres.
Take a long glass fibre and fasten to it a mirror from which a spot of
light is reflected on to a scale, twist the fibre about its axis and keep it
twisted for a considerable time. Then remove the twisting couple : the
spot of light will at once come back a considerable distance towards its old
position, but will not reach it, and the rest of the journey will be a slow
creep towards the old position, and several hours may elapse before the
journey is completed. The larger the initial twist and the longer the
time for which it was applied the greater is the tempoi-ary deflection of
the spot of light from its original position.
The general shape of the curve which represents the relation between
the displacement of the zero — i.e., the displacement of the position of the
spot of light — and the time which has elapsed since the removal of the
twist, is shown in Fig. 24. In this cui-ve the ordinates represent the
displacement and the abscissse the time since the removal of the twist.
The altitude PN, when the abscissa ON is given, depends upon the
56
PROPERTIES OF MATTER.
magnitude of the initial twist and the time for which it was applied ; the
curve is steep at first but gets flatter and flatter as the time increases.
The longer the initial twist is applied the more slowly does the zero
approach its original position. Yery complicated movements of the zero
may occur if the fibre has been twisted first in one direction and then
in the opposite for a considerable number of times. The general features
of this phenomenon will be illustrated by the following simple case. Suppose
that immediately after the removal of the first twist, whose after-effect,
if it were alone, would be represented by the curve (I), Fig. 24, a second
twist in the opposite direction is applied for a time represented by ON and
then removed. Suppose that the deflection of the zero due to this twist
alone is represented by the dotted curve (II) (as the twist is in the opposite
2V K
Pig. 24. — Curve showing the Elastic After-effect in a Twisted Glass Thread.
direction, the ordinates represent negative deflections). Then if we can
superpose the efiects, the displacement of the zero at a time NK after the
removal of the second twist will be represented by the differences between
the ordinates KR, KS of the two curves. The ordinate of the second curve
may be above that of the first at the time tlie second twist is removed, and
yet, as the curve is very steep just after the removal of the twist,
curve (II) may drop down so quickly as to cut the first, as shown in the
figure. Thus in this case we should have the following effects: immediately
after the removal of the second twist there would be a displacement of
the zero in the direction of the last applied twist, the spot of light would
then creep back to the zero but would not stay there, but pass through
the zero and attain a maximum deflection on the other side ; it would then
creep back to the zero and would not again pass through it. In this
way, by superposing twists of difierent signs, we can get very complicated
movements of the zero, which are a source of trouble in many instruments
which depend upon the torsion of fibres. With quartz fibres the residual
ELASTICITY.
57
effect^is^exceedingly smaLl, and this is one of the chief causes which make
their use so valuable. The residual after-effect in glass is a cause of
trouble in thermometry, each change of temperature causing a temporary
change in the zero.
The magnitude of the elastic after-effect seems to increase very greatly
when~ there is^ a want of homogeneity in the
constitution of the^ body. In the most homo-
geneous bodies we know, crystals, it is exceedingly
small, if it exists at all, while it is very large in
glass which is of composite character, being a
mixture of different silicates ; it exists in metals,
although not nearly to the same extent as in
glass. A similar dependence upon want of
uniformity seems to characterise another similar
effect — the residual charge of dielectrics {see
volume on Electricity and Magnetism), the laws
of which are closely analogous to those of the
I elastic after-effect.
The phenomenon of elastic after-effect may
be illustrated by a mechanical model similar to
that shown in Fig. 25.
A is a spring, from the end, B, of which
another spring 0 is suspended, carrying a
Fig. 25.
damper D, which moves in a very viscous
liquid. If B is moved to a position B' and kept
there for only a short time, so short that D has
not time to move appreciably from its original
position, then when B is let go it will return at
once to its original zero, for D has not moved, so
that the conditions are the same as they were
before B was displaced. If, however, B is kept
in the position B' for a long time, D wiU slowly move off to a position D',
such that D' is as much below B' as D was below B. If now B' is let go
it will not at once return to B, for in this position the spring between B
and D is extended, B will slowly move back towards its old zero, and will
only reach it when the slow moving D' has returned to D.
Viscosity of Metals and Elastic Fatigue.— If two vertical wires,
one made of steel and the other of
zmc.
O'
FlO. 26.
are of the same length and
diameter, and carry vibration bars
of the same diameter, then if
these bars are set vibrating the vibrations die away, but at very different
rates : the steel wire will go on vibrating for a long time, but the zinc
wire will come to rest after making only a small number of vibrations.
This decay in the vibrations of the wire is not wholly nor even mainly
due to the resistance of the air, for this is the same for both wires ; it is
due to a dissipation of energy taking place when the £arts of a metal wire_
are in relative motion, and may, from analogy with the case of liquids
and gases, be said to be due to the viscosity of the metal. We can
see that elastic after-effect would cause a decay in the vibrations of
the wire. For suppose 0, Fig. 26, represents the original zero — i.e., the
place where the force acting on the system vanishes, then if the wire is
5d
PROPERTIES OF MATTER.
displaced to A and then let go the new zero will be at 0', a point between
A and 0 ; thus the force will tend to stop the vibration as soon as the
.<>•
^
Fig. 27.
I'iG. 2«.
wire passes 0' — sooner, that is, than it would do if there were no after-
effect. Again, when the wire is on the other side of 0, the zei'o will be
displaced by the elastic after-effect to O", a point between 0 and B, and
thus again the force tending to stop the vibration will begin to act sooner
than it would if there were no
elastic after-effect. "We can see the
same thing from the study of the
model in Fig. 25, for some of the
kinetic energy will be converted into
heat by the friction between the
viscous fluid and the damper D.
Lord Kelvin discovered a remark-
able property of the viscosity of
metals which he called elasticj^aligue.
He found that if a wTre^ were~kept
vibrating almost continuously the
rate at which the vibrations died
away got greater and greater ; in
fact, the wire behaved as if it got
tired and could only with difiiculty
keep on vibrating. . If the wire
were given a rest for a time it
recovered itself, and the vibrations
for a short time after the rest did
not die away nearly so rapidly as
they had gone just before the rest
jPjq 29 began. Muir {Proc. Roy. Soc, Ixiv.
p. 337) found that a metal wire
recovered from its fatigue if it were warmed up to a temperature above
100° c.
Anomalous Effects on first Loading* a Wire.— The extension pro-
duced by a given load placed on a wire for the first time is not in general
quite the same as that produced by subsequent loading ; the wire requires
ELASTICITY.
59
to be loaded and unloaded several times before it gets into a steady state.
The first load after a rest also gives, in general, an irregular result. It
seems as if straining a wire produced a change in its structure from which
it did not recover for some time.
Great light will probably be thi'own on this and the other effects we
have been considering by the examina-
tion by the microscope of sections of
the metals. Wli^n examined in this
way it is found that metals possess a
structure coarse enough to be easily
rendered visible. Figs. 27, 28, 29
show the appearance under the micro-
scope of certain metals. It will be
seen from these figures that in these
metals we have aggregates of crystals
of very great complexity— the linear
dimension of these aggregates is some-
times a considerable fraction of a
m'llimetre. These large aggregates
arc certainly altered by large strains.
Thus Ewing and E,osenhain (Proc.
Roy. Soc, xlv. p. 85) have made the
very interesting discovery that when a metal is strained past its yield-
point thereis a slipping of the crystals, which build ujg^ the aggregates
along tbeiFpTanes of cleavage. The appearance of a piece of iron after
straining" past the yield-point is shown in Fig. 30 ; the markings in
the figure are due to the steplike structure of the aggregates caused
Fio. 30.
Before straining.
, , , y I I I I I I I -
After straining.
Fia. 31.
by the slipping past each other during the strain of the crystals in
the aggregates, as in Fig. 31. Plasticity may tlius be regarded as the
yielding, or rathei^ slipping past each other of the-jrystals of the large
J^ggJ^egatesjwhich the^microscope shows exist in metals.
'^In harmony with this view is the observation of McConnel and Kidd
{Proc. Hoy. S'oc, xliv. p. 331) that ice in mass is plastic when consisting of
crystals irregularly arranged. In later experiments {Proc. Roy. Soc, xlix.
p. 323), McConnel found that a single crystal of ice is not plastic under
pressure applied along the optic axis, but that it does yield under pressure
6o
PROPERTIES OF MATTER
inclined to the axis, as if there were slipping of the planes perpendicular
to the axis.
If there is a general change in these aggregates under large strains it
is possible that there are soine_aggregates,\vhich are unstable eijough to
be broken up by smaller"^trains, and that the first application is accom-
panied byXbreaking^up^f some^fjbhe^nore unstable groups, so that the
structure of thejm^al_jsJligMlx^^"g^^ ^® ^^ *^^®° understand the
irregularities^ observed when a wire is first loaded and also the existence
of the elastic after-eflect. Indeed, it would seem almost inevitable that
any strain among such irregular-shaped bodies as those shown in Fig. 28
would result in some of them getting jammed, and thus becoming exposed
to very great pressures, pressures which might be sufficient to break up
some of the weaker aggregates, and thus give relief to the system. The
existence of such a structure as that shown in Fig. 28 causes us to
wonder whether, if a succession of very accurate observations of the
elastic properties of a metal were made, the results would not difler
from each other by more than could be accounted
for by the errors of experiment.
The term viscosity is often used in another
sense besides that on p. 57. We call a substance
viscous if it cannotresist the application or a
small force actingj^oi^a long time. Thus we call
prtcE"vIscous because, if given a sufiiciently long
time, it will flow like water ; and yet pitch can
sustain and recover from a considerable force if
this acts only for a short time. Fig. 32 shows
the way in which some very hard pitch has
flowed through a vertical funnel in which it has
been kept in the Cavendish Laboratory for nine
years. In an experiment, due to Lord Kelvin,
pieces of lead placed upon a plate of pitch found
in course of time their way through the plate.
Many substances, however, show no trace of
viscosity of this kind, for the existence of sharp
impressions on old coins, the preservation of
bronze statues and the like, show that metals can
sustain indefinitely (or at any rate so nearly
indefinitely that no appreciable change can be detected after thousands of
years) their shape even under the application of small forces.
Breaking- of Wires and Bars by Tension.— The following table,
due to Wertheim, gives the load in kilogrammes per square millimetre
necessary to break wires of difierent substances :
Fio. 82.
Lead .
. 21
Copper
. 40-3
Tin .
. 2-5
Platinum .
. 341
Gold .
. 27
Iron .
. Gl
Silver .
. 29
Steel Wire .
. 70
Zinc .
. 128
The process of drawing into wire seems to strengthen the material,
and the finer the wire the greater is the pull, estimated per unit araa of
cross section, required to break it. This is shown in the following table
given by Baumeister (Wiedemann, Annakii, xviii. p. C07) :
Material.
Swedish Iron
»>
i»
n
j>
Brass
a
n
>»
n
>>
ELAS
Ticny.
Diameter of wire ^"" ^" kilogramrres
x^iaiiietci ui wiiB ^^^^ required
^" ™°"- to break the wire.
. -72
. Gi
•50
83
•30
96
•25
94
•15
98
■10
123
•75
76
. ^25
. 98
. •lO
. 98
61
The efl'ect of temperature on the pull required to break a wire is com-
plex. Iron wire shows several maxima and minima between 15° C.
and 400° C. (Pisati, Bend. Ace. Lincei. 1876, 76); the strength of copper,
on the other hand, steadily diminishes as the temperature increases.
The strength of a material is sometimes very seriously affected by the
addition of only a small quantity of another substance. Thus Sir William
Roberts-Austen found that gold, to which 2 per cent, of potassium had
been added, could only sustain 1/12 of the weight required to break
pure gold. In the case of steel, the addition of small quantities of carbon
to the iron increases the strength. The microscopical examination of the
structure of metals, such as is shown in Figs. 27—30, may be expected to
throw a good deal of light on effects of this kind. In this way it has been
shown that the foreign substance is sometimes collected between the
aggregates of the crystals of the original metals forming a weak kind of
mortar, and thus greatly reducing the strength of the metal. In other
cases, such as steel, a carbide is formed, and the appearance of a section
of the steel under the microscope shows that the structure is much
finer than in pure iron. It would seem from Sir William Roberts-Austen's
experiments that the addition to gold of a metal of greater atomic volume
than the gold diminishes, while a metal of smaller atomic volume increases
the strength.
CHAPTER V.
STRAIN.
Contents. — Homogeneous Strain — Principal Axes of Strain — Pure Strain —
Elongation — Dilation or Compression — Contraction — Shear — Angle of Shear.
"When a body changes in shape or size it is said to be strained, and the
deformation ot the bodyis called strain.
HomOgreneOUS Strain. — We shall restrict ourselves to the most simple
class of strain to which bodies can be subjected ; this is when any two lines
which are equal and parallel before straining remain equal and parallel
after straining. This kind of strain is called homogeneous strain.
Thus by a homogeneoua strain a parallelogram is strained into another
parallelogram, though its area and the
altered by straining ;
angle
parallel planes strain
B
between its sides may be
into parallel planes, and
Fig. 33.
parallelepipeds into parallelopipeds. Figures which are similar before
straining I'emain similar after the strain.
It follows from the definition of homogeneous strain that the ratio of
the length of two parallel lines will be unaltered by the strain. Let AB
and CD (Fig. 33) be two parallel lines. Let the ratio of A B to CD be m : n.
Then, if m and n be commensurable, we can divide AB and CD respectively
into Nm and N«, equal parts each equal to a. Then, as before straining all
these parts are equal and parallel, they will remain so after a homogeneous
strain. Thus AB, after straining, will consist of Nm and CD of Nn parts,
each equal to a ; and the ratio of the strained lengths is m : w, the same
as that of the unstrained lengths. If m and n are not commensurable we
can deduce the same result in the usual way by the method of limits.
From this result we can at once prove that a sphere is strained into an
ellipsoid, and that three mutually perpendicular diameters of the sphere
STRAIN.
63
strain into three conjugate diameters of the ellipsoid. As some of our
readers may not be familiar with solid geometry, we shall confine our
attention to strains in one plane and pi'ove that a circle is strained into
an ellipse; the reader who is acquainted with solid geometry will not
have any difiiculty in extending the method to the case of the sphere.
Let ABA'B' (Fig. 34) be a circle, centre 0, which strains into aba'b',
corresponding points on the two figures being denoted by corresponding
letters. Let P be a point on the circle, PL and PM parallel to CA
Fm. 34.
and CB respectively; let these lines on the strained figure be denoted
by pi, pm.
Thus, since the ratio of parallel lines is not altered by the strain
PL^pZ
CA ca _
PM _pm
CB'^cb
But since P, A, B are on a circle whose centre is 0
1
PL2 PM^
hence
ca- CO-
OT p is on an ellipse of which ca and cb are conjugate diameters. Thus
a circle is strained into an ellipse, and two diameters at right angles to
each other in the circle strain into two conjugate diameters of the ellipse.
Now there are two, and only two, conjugate diameters of an ellipse
(unless the ellipse degenerates into a circle) which are at right angles to
each other. Hence there are two, and only two, diameters at right angles
to each other before straining which remain at right angles after the strain.
Now, though in general these diameters will not have the same direction
64
PROPERTIES OF MATTER.
after straining as they had before, yet we shall not be introducing any
real limitation on the strain in so far as it affects the forces called into play
by elasticity if we suppose they retain the same direction after straining
as before. For, suppose OA, OB (Fig. 35), are the unstrained directions,
Oa, Ob, the strained ones, we can make Oa, 06 coincide with OA, OB by
rotating the strained system as a rigid body through the angle AOa.
This rotation as a rigid body will not involve any relative motion of the
parts of the system, and so will not call into play any forces depending
upon the elasticity of the system ; if, then, as is at present the case, our
object is to investigate the connection between these forces and the strains,
we may leave the rotation out of account.
The three directions at right angles to each other which remain at right
angles to each other after sti\aining are called the principal axes of strain.
If these axes have the same direction after straining as before, the strain
is said to be a pure^trainj
if it requires a rotation to
make the principal axes
after straining coincide
with their position before
the strain, the strain is
said to consist of a pure
strain and a rotation.
Thus the most general
homogeneous strain may
be resolved into extensions
(regarding a compression
/j as a negative extension)
Fig. 35. along three directions at
right angles to each other,
fake these directions as the axes of x, y, z respectively, then if a line of
unit length parallel to the axis of x has, after the strain, a length 1+e ;
one parallel to the axis of ?/ a length 1 +/; and one ♦parallel to the axis of »
a length 1 + g', e, f, g are called the principal elongations. If e =/= g,
then a sphere strains into a sphere, or any figure into a similar figure,
the strained figure being an enlarged or diminished copy of the unstrained
one. These cases, which are called uniform dilatation or compression,
involve changes in size but not in shaped
A cube whose sides were parallel to the axes before straining and one
unit in length becomes after straining a rectangular parallelepiped, whose
edges are 1 + e, 1 +/, 1+9' respectively, and whose volume is (1+e) (1 +f)
(1 +g). If, as we shall suppose all through this chapter, the elongations
e, y, g are such small fractions that the products of two of them can be
neglected in comparison with e, f, or g, the volume of the parallelepiped
is l+e+Z+gr.
Hence the increase of unit volume due to the strain is e+f+g. This
is called the cubical dilatation . We shall denote it by I, and we have
l-'e+f+g.
If the strain is a uniform dilatation e=f=g, and therefore
CO that in this case the cubical expansion is three times tb» linear elongation.
STRAIN.
65
Resolution of a Homogfeneous Strain into Two Strains, one of
which chang-es the Size but not the Shape, while the other
changfes the Shape but not the Size.
Let us consider the case of a strain in one plane. Let OA, OB (Fig. 30)
be the principal axes of strain. Let P be the initial position of a point, P' its
position after the strain. Then if e,fixve the elongations parallel to OA and
OB, '£, and rj the displacements of P parallel to OA and OB respectively,
; = eON = i (e +/)0N + i(e -/)0N,
„ =/0M = h{e +/)0M - i(e -/)0M.
From these expressions wc see that we may regard the strain e, f
as made up of a uniform ^
dilatation equal to -v(e+/),
together with an elongation
i(e -/) along OA, and a con-
traction ^(e -/) along OB.
Thus the strain superposed
on the uniform dilatation con-
sists of an expansion along
one of the principal axes and
an equal contraction along
the other. This kind of strain
does not alter the size of the
body ; for if a is the elonga-
tion along OA and the con-
traction along OB, then a
square whose sides are one unit in length and parallel to the principal
axes becomes a rectangle whose sides are 1 -1- o-, and 1 - o- respectively ; the
area of this lectangle is 1 - ff", or since we neglect the square of o- the area
is unity, and thus is not altered by the strain. A strain which does not
alter the size is called a shear. Thus any strain in one plane can be
resolved into a uniform dilatation and a shear.
We have considered a shear as an extension in one direction and an
equal compression in a direction at right angles to this ; there is, however,
another and more usual way of considering a shear, which may be deduced
as follows :
Let OA, OB (Fig. 37) be the axes along which the extension and
contraction take place. Let OA == OB = OA' = OB' = 1 , so that before
straining ABA'B' is a square ; let this square after straining be represented
by aha'b', which will be a parallelogram.
Since Oa = 1 + <r
06 - 1 - <r
ah' = 2 + 2(7-'
= 2
as we suppose that o- is so small that its square may be neglected. Thus
a6 = AB. Hence we can move aha'h' as a rigid body and place it so that a6
coincides with AB, as in Fig. 38. Then, since the area of aba'h' is equal to
that of ABA'B', when the figures are plactd so as to have one side in common
E
(i6
PROPERTIES OF MATTER.
they will lie between the same parallels. Thus, if a"6" be the position of a'V
when ah is made to coincide with AB, a"b" (Fig. 38) will lie along A'B' ;
hence, except with regard to the rotation, the expansion along AO and the
Fig. 37.
contraction along OB is equivalent to the strain which would bring ABA'B'
into the position ABa"6". But we see that this could be done by-
keeping AB fixed and sliding
every point in the body par-
allel to AB through a distance
proportional to its distance
from AB. We can illustrate
this kind of strain by a pack
of cards lying on the table,
with their ends in vertical
■^ planes ; now slide the cards
forward, keeping the lowest
one at rest in such a way
that the ends are still flat
although the planes are no
longer vertical ; each card
will havebeen moved forwards
through a distance propor-
tional to its distance from the
lowest card . The angle A'Ba"
tliroiigh which a line is dis-
placed which to begin with is perpendicular to AB is called the angle of
shear. The plane of the shear is a plane parallel to tbe_ direction of
motion anci at riglit angles to theirxecTpIane.
' The relation between y — tlie circular measure of the angle of shear — and
the elongation a along OA, and the contraction it along OB can be found as
follows. Before the rotation making ah coincide witli Al), ha! makes
with BA' the angle B^6 ; to make ah coincide with AB (Fig. ^7) the system
has to be rotated through the angle Bp6, so that after the rotation ha will
Fig. 33.
STRAIN. 67
make with BA' the angle B^^ + Bpb. Now by the figure, Bqh = Rph, hence
the angle of shear is 2 L liqb = 2 ^apA. If Am is perpendicular to ap (Fig. 37),
then, since the angle apA is by hypothesis small, its cii'cular measure
Km _ A(xsin45 Aa_
^Tp^ TaojW "ao""'
hence d, the circular measure of the angle of shear, = 2<r.
If e and / are the extensions along two principal axes in the genei'al
case of homogeneous strain in two dimensions, we see from p. G5 that this
strain is equivalent to a vmiform dilatation ^ (e +/) and to a shear the
circular measure of w^hose~angle Is e —f, '~
CHAPTER VI.
STRESSES. RELATION BETWEEN STRESSES AND STRAINS.
Contents. — General Considerations — Hooke's Law — Work required to produce any
Strain — Rectangular Bar acted upon at Right Angles to its Faces.
^71.
In order that a body may be strained forces must act upon it. Consider a
small cube in the middle of a sti-ained solid, and suppose for a moment that
the external forces are confined to the surface of this solid. Then the forces
which strain this cube must be due to the action exerted upon it by the
surrounding matter. These forces, which are due to the action of the
molecules outside the cube on those inside, will only be ajjpreciable at
molecular distances from the surface of the cube, and may therefore
without appreciable error be supposed to be confined to the surface. The
most general force which can
act on a face ABCD of the
cube may be resolved into
three components, one at right
angles to ABCD, the other
two components in the plane
of ABCD, one parallel to AB,
the other to BC : similarly
over the other faces of the
cube we may suppose similar
forces to act. These forces
are called stresses ; the com-
ponent at right angles to a
face is called a normal stress,
the component parallel to the
Fig. 39. face a tangential stress. The
intensity oi any component of
the stress is the amount of the component over the face divided by the
area of the face. We shall for brevity leave out the word " intensity^'
and speak of it simply as the stress. The dimensions of a stress are those
of a force divided by an area or M/LT-. It is measured in dynes per
square centimetre ; on the C.G S. system of units the pressure of the
atmosphere is about 10" units of stress.
When we know the stresses over three planes meeting at a point O
(Fig. 40) we can determine the stresses on any other plane through O. For
let OABC be a very small tetrahedi-on, AOB, BOC, COA being the pianos
over which we know the stresses, and ABC being parallel to the plane across
which we wish to determine the stress. Then as this tetrahedron is in
equilibrium under the action of forces acting on its four faces, and as we
/>k^- y.
STRESSES.
fin
1
know the forces over three of the faces, OAB, OBC, OCA, we can
determine the force, and hence the stress, on the fourth. We need not
take into account any external forces which are proportional to the volume
on which they act, for the forces due to the stresses are proportional to the
area of the faces, that is, to the square of the linear dimensions of the
tetrahedron, while the external forces are proportional to the cube of the
linear dimensions, and by making the linear dimensions of the tetrahedron
exceedingly small we can make the eflect of the volume forces vanish in
comparison with that of the surface forces.
The stresse§_in a strained solid constitute a system of forces which are
in equilibrium at each part of the solid with the external forces acting"o"n
the solid! If we call the external forces the load, then if a load W pro-
duces a system of stresses P,
and a load W a system of
stresses P', then when W and
W act together the stresses
will be P + P' if the deforma-
tion produced by either load
is small.
Hooke's Law.— The fun-
damental law on which all
applications of mathematics
to elasticity are based is due
to Hooke, and was stated by
him in the form ut tensio sio
vis, or, in modern phraseology,
that tjif gfraiy^s are propor-
tional to the loads. The truth
ot this law, when the strains
do not exceed the elastic limit
(see p. 53), has been verified
by very careful experiments
on most materials in common
use. Another way of stating Fio. 40.
Hooke's Law is that if a load
W produces a strain S, and a load W a strain S', then a load W + W will
produce a strain S + S'. Hence, it follows from the last article that if a
system of stresses P correspond to a system of strains S, and a system of
stresses P' to a system of strains S', then a system of stresses P -|- P' will
correspond to a system of strains S -|- S'. Hence, if we know the stress
corresponding to unit strain, we can find the stress corresponding to a
strain of any magnitude of the same type. Thus, as long as Hooke's law
holds good, the stress and strain will be connected by a relation of the
form
Stress = c X strain
where c is a quantity which does not depend either upon the stress or the
strain. It is called a modulus of elasticity. Thus, if the strain corresponds
to a change in size but not in shape, then the stress is a uniform pressure,
and the strain the diminution in volume of unit volume of the unstrained
substance ; in this case c is called the modulus of elasticity of bulk, or
jnore frequently the bulk modulus. Again, il" the strain is a shear wliich
w
>{k
70
PROPERTIES OF MATTER.
.-^<
^ . alters the shape but not the size, the strain is measured by the angle of
^-r"^^^ shear and the stress by the tangential force per unit area, which must bo
applied to produce this sliear. In this case c is called the modulus of
rigidity. If we stretch a wire by a weight, the stress is the weight divided
by theiuea of cross section of the wire, the strain is the increase of length
in unit length of the wire, and in this case c is called Young's modulus.
Since we can reduce the most general system of homogeneous strain to
a uniform expansion or contraction and a system of shears (see p. 65) it
follows that if we know the behaviour of the body (1) when its size but not
its shape is changed, and (2) when its shape but not its size is changed, we
can determine its behaviour under any homogeneous strain. This is true
when, and only wlien, the properties of the substance are the sjime in all
directions, so that a uniform hydrcstatic pressure produces no change in
L ^f JV
Fig. 41.
shape, and the tangential stress required to produce a given angle of shear
is independent of the plane of the shear. This statement is equivalent to
saying that it only requires two moduli — i.e., the bulk modulus and the
modulus of_iigiclitv. to tix the elastic behaviour of the substance, so that all
other moduli, such as Young's modulus, must be expressible in terms of
these two.
Work required to produce any Strain.— The result for the most
general case, and the method by wliich it can be obtained, may be illus-
trated by considering the work required to stretch a wire. Let us suppose
that the load is added so gradually that the scale-pan in which the weighta
are placed never acquires an appreciable velocity, so that none of the work
done is converted into kinetic energy, but all is spent in stretching the
wire. When this is the case, the weight in the scale- pan when in any
position never exceeds by more than an infinitesimal amount the weight
required to stretch the wire to that position.
Let the straight line AB, Fig. 41, represent the relation between
the weight in the scale-pan and the extension of the wire, the
weight being the ordinate and the extension the abscissa ; let OA repre-
STRESSES. 71
eent the unstretched length of the wire. Consider the work done
in stretching the wire from L to M, where L and M are two points veiy
near together. The force will be approximately equal to PL ; thus
the woi-k done in stretching from L to M will be PL x LM — i.e., the
area PLMQ' ; similarly, the work done in stretching the wire from M to N
will be represented by the area QMNIl', and thus the work spent in
stretching the wire from OA to OG will be repiesented by the sum of the
little rectangular areas ; but when these rectangular areas are veiy small,
their sum is equal to the area ABO, and this equals iBO x AC — i.e., one-
half the final weight in the scale-pan x extension of the wire. Let a be
the area of cross section of the wire and I the length, then EC ■=« x stress
and AC = ^ X strain. Thus the work done in stretching the wire is equal
to al X I strain x stress. Now al is the volume of the wire, hence the
energy in each unit volume of the wire is -J strain x stress. Though we
have considered a special case, it will be seen that the method is of general
application, and that the result will hold whenever Ilooke's law is true.
We have considered two ways of regarding a shear : one where the
paiticles of the body were pushed forward by a tangential force as is
represented in Fig. 38. In this case the work done on unit volume, which
is the energy possessed by the sheared body, is
where T is the tangential force per unit area and d the angle of shear.
The other way of regarding a shear is to consider it as an extension in
one dii'ection combined with an equal contraction in a direction at right
angles to the extension. Let e be the magnitude of the extension or
contraction, P the pull per unit area producing the extension ; this is equal
to the push per unit area producing the contraction. Considering unit
volume of the strained body, the work done by the pull is | Pe, and that
by the push is also ^ Pe; hence the energy per unit volume is ^ Pe + ^ Pe = Pe,
but this energy is also equal to J Td, hence
Pe = lT0.
But we know (p. 67) that d = 2e, hence
P = T.
Hence the pull or push per unit area in the one way of considering a
shear is equal to the tangential stress per unit area which occurs m tEe
other way.
it n IS the coefficient of rigidity, then by the definition of n given on
p. 70,
T = n6
hence P = 2ne
P
or 6 = —
2n
Rectangular Bar acted on by Forces at Right Angles to its
Faces. — Let ABCDEFGH, Fig. 42, be a rectangular bar Let the
faces CDEF, ABGH be acted on by normal pulls equal toP per unit area,
the faces A BCD, EFHG by normal pulls equal to Q per unit area, and the
faces DEGB, CFHA by normal pulls equal to R per unit area. We shall
72
PROPERTIES OF MATTER.
proceed to find the deformation of the bar. Considering the bar .^s made
up of rectangular pai-allelopipeds, with their faces parallel to the bar, we see
that these Avill all be in equilibrium, whether they are in the interior of the
bar or whether some of their faces are on the surface of the bar, if the
normal stresses parallel to AC, CD, DE are respectively equal to P, Q, R,
and if there are no tangential stresses. Each of these parallelepipeds will be
subject to the same stresses, and will therefore be strained in the same
way. Let e,/, g be the extensions parallel to P, Q, R respectively. Con-
sider for a moment what the strains
would be if the stress P acted alone : P
would produce an extension proportional
to P in the direction of P ; let us call
this XP; it would also produce contraction
proportional to P in any direction at
right angles to P ; and if the properties
of the strained substances were the same
in all directions, then the contractions
would be the same in all directions at
right angles to P ; let these contractions
"^"be yuP. Then when P acts alone the
extensions parallel to P, Q, R respectively
are XP, - juP, - /iP ; similarly when Q
acts alone the extensions in these directions
are -/iQ, XQ, -juQ, and when R acts
alone the extensions are - fxR, - /iR, XR ;
consequently when these stresses act simul-
taneously we have
e = XP - yuQ - ^iR"
/=-^P + XQ-^R
g= -^iP-^Q + XR
(1)
Now we have seen (p. 70) that the
elastic pi-operties of the substance are
completely defined if we know the bulk
rio. 42. modulus, which we shall denote by k, and
the modulus of rigidity which we shall
denote by n. Hence we must be able to express X and ^ in terms of n
and k. We proceed to do this. If we apply a uniform tension to each
side of the bar equal to P the dilatation of unit volume is equal to Vjk,
by the definition of k ; but in this case the dilatation is uniform in all
directions, and the linear dilatation is one-third of the volume dilatation
— i.e., it is equal to Tj^k.
p
Hence, when P = Q = R, e=/=gr = _-,
ok
hence, from equations (1) -- = X - 2/t.
ok
Let us now shear the body in the plane of PQ — i.e., put Q = - P and
R = 0. In this case e= -/= P/2n (see p. 71) ; hence by equations (1)
2^-'+'-
STRESSES. 73
l>ink
g = l{^-a{V + q)\
If the bar is prevented from contracting laterally,
hence Q = R = ,
1 — ff
P/ 2er2
80 that e = — 1 - - —
- ' o \ 1 - c
/ ^,
3\?i o^/ 'J7^^
Yoiing''s Modulus. — A very important case is that of a bar acted on
by a pull parallel to its length, while no forces act at right angles to the
length. In this case Q = R = 0, and we have
e = XP,/= -/zP,r/=-yuP.
But in this case the stress, divided by the longitudinal strain, is called
Young's modulus ; hence, if we denote Young's modulus by q, we have,
This equation gives Young's modulus in terms of the bulk modulus and
the rigidity.
PoiSSOn's Ratio. — Poisson's ratio is defined to be the ratio of the
lateral contractiPiTto the longitudinal extension for a^ar acted on by a
stress parallel to its length. If we denote it by <r, then by this definition
f
9-= -^, when Q = R = 0. __ _ ^.7
Thus (T = " = —r—, — -^ .
\ 2{U + n)
Since n is a positive quantity, we see from this expression that c must
be less than 1/2. According to a molecular theory worked out by Cauchy
and Poisson, o-, for all non-crystalline substances, is equal to 1/4. The
determinations of or given in the table of elastic constants on p. 102 do
not lend much support to this view.
Bar stretched long-itudinally, with its Sides fixed.— The
equations (1) may be written
«=lfp-<T(Q + Il)
q\
9\
74
PRO PR [{TIES OF MATTER.
B
Hence the elongation is less than if the sides of the bar were free in
the ratio of 1 - , — - to 1. In the case of a steel bar for which o- = -268
i. — a
the elongation if the sides were fixed would be about 4/5 of the elonga-
tion when the sides are free.
Determination of Young^'s Modulus. — A simple way of measuring
Young's modulus for a wire of which a considerable length is
available is the following : Fix as long a length of the wire
AB, Fig. 4;-i, as is available firmly to a support. Another
wire, CD, which need not be of the same material, hangs from
the same suppoit down by the side of the first wire. CD
carries a millimetre scale, the length of the scale being parallel
to the wire ; a weight is attached to the end of this wire to
keep it straiglit. A vernier is attached to the wire AB and
moves against the scale fixed to the wire CD. The wire AB
carries a scale-pan into which various weights can be placed.
By reading the vernier when different weights are on the
scale-pan we get the vertical depression of a fixed point on the
vernier, that is of a known point on the wire, produced by a
given weight. Let this depression be e, when the weight in
the scale-pan is increased by W. Measure the length of the
wire between the fixed support and the point of attachment to
the vernier ; let this be I, then the elongation per unit length
is til. If w is the cross section of wire, then the stress which
produces this elongation is W/'w, so that, as Young's modulus
is stress divided by strain, it is equal to
To determine the cross section, the most accurate way is to
weigh a known length of the wire, first in air and then in
water. The difierence of the weighings in grammes will be
the volume of the wire in cubic centimetres, and if we divide
the volume by the length we get the cross section. Preliminary
measurements should have been taken with a screw gauge to
see that the wire was uniform in section. It is advisable to
load and unload the wire several times before making the final
measurements. This serves to straighten the wire, and avoids
the anomalous results which, apart from straightening, are
obtained when a wire is loaded for the first time after a rest.
Fig. 43. We owe the following improvements of this method to Mr.
G. F. C. Searle. Two brass frames, CD, (d'\y. Fig. 44, hang from
the lower ends of the wires and support the two ends of a sensitive level L.
One end of the level is pivoted to the frame CD by the pivots H, the
other end of the level rests upon the end of a vertical screw S working in
a nut attached to the frame CD'. The two links, K, K', prevent the
frames from twisting relatively to each other about a vertical axis, but freely
allow vertical relative motion. When these links are horizontal the two
wires are parallel to each other. A mass M and a pan P hang from the
lower ends of the frames, and the weights M and P are suflicient to
straighten the wires. The connections between the wires and the frames
STRESSES.
75
are made by the swivels F, into which the ends of the wires are soldered.
The swivels prevent the torsion o? the wire. The head of the screw is
divided, say, into 100 parts, while the pitch of the screw may be "5 mm.;
thus each division on the head corresponds to 1/200 mm. The
measui'ements are made in the following w^ay : Adjust the screw so that
one end of the bubble is at zero; if a weight be placed in the pan P the
Fig, 44.
wire A' is stretched, and the bubble moves towards H ; bring the bubble
back to zero by turning the screw ; the distance through which the screw
is moved is equal to the extension of the wire.
When the substance for which Young's modulus is to be determined
is a bar and uot a wire, the extensions obtained by any practicable weight
would be too small to be measured in the way just desciibed. In this case
Ewing's extensometer may be used. This instrument is represented in
Fig. 45. A is the rod whose extension is to be measured, B and C
are pieces attached to A by set screws about the axes of which they
revolve; the arm B' fixed to B ends in a rounded point P, which fits
into a V-shaped slot cut transversely across the end of the piece C
76
PROrERTIES OF MATTER.
' \
Si
Thus, when the rod A is stretched, the point P acts as a fulcrum, and
Q, the opposite end of C, moves down through a distance proportional
to the extension between the axes of the set screws. The displacement of
Q is PQ/OP times the extension of the bar. This displacement is observed
by a microscope which is attached to the bar B, and sights an object
at Q. The displacement is measured by means of a mici'ometer scale en-
graved on glass in the eye-piece of the microscope ; extensions of 1/20,000
of a centimetre are readily measured in this way. There is a fine screw,
with a divided head between B' and the point P. This serves to bring Q
into a convenient position for sighting, and also to determine what is
-.^"C
Fig. 46.
the absolute amount of extension corresponding to a division of the
eye-piece scale ; for if we know the pitch of the screw we know the dis-
placement of Q when the screw-head is turned through one revolution ;
if we find how many divisions of the micrometer scale this corresponds
to we can at once standardise the scale. The pull is applied to the bar
by means of a small testing machine.
Optical Measurement of Young-'s Modulus. — Michelson's method
of interference fringes, produced by the aid of semi-transparent mirrors,
gives a very delicate way of measuring small extensions.
The principle of the method is shown in Fig. 46. A and B are plane
plates of very carefully worked glass of the same thickness. One surface of
A is coated with a tliin film of metal, preferably platinum. The platinum
may be deposited on the glass by placing the glass near a platinum
cathode in an exhausted tube, and sending a current from an induction
STRESSES.
77
coil through the tube. The platinum sputters from the terminal and is
deposited on the glass. This film is so thin as to be semi-transparent ; it
allows part of the light to pass through it. Suppose a beam of light,
starting from S, falls on the plate A, some of it is reflected from the
upper surface of the plate, and after being reflected from the mirror C
returns and passes out of the plate A and enters the eye at E ; another
part of the beam passes through the plate A, is reflected at D, returns to
the plate A, where it is reflected to E. Even when the difierence of path
is great, if A and B are very truly plane and of the same thickness the first
part of the beam from Swill interfere with the second part and produce inter-
ference bands. If the distance between one of the mirrors and the plate A is
D
E
Fig. 4«,
altered, the bands are shifted ; an alteration of the distance through 1/4 of
a wave-length will make the dark bands and light bands interchange
their position ; by observing the position of the bands we can measure
movements of the mirror amounting to 1/50 of the wave-length of sodium
light, or say a millionth of a centimetre. To apply this method to the
determination of Young's modulus we keep one of the mirrors fixed while
the other is cari'ied by the wire whose extension we wish to measure.
Since we can measure accurately in this way very small extensions we are
able to use comparatively short wires, and so have all the conditions of
the experiment under much better control than when a long wire is
used. This method has been used by Mr. Shakespear at the Cavendish
Laboratory. He has also used the method described on p. 43 for multi-
plying the small movements of the pointer of a balance, to multiply the
movement due to the extension of a wire.
Other methods of detej'mining q will be given in the chapter on the
Bending of Rods.
CHAPTER Vli.
TORSION.
Contents. — Torsion of Circular Tabes and Hods— De St. Venanf s Researches—
ytatical and Dyuumical Methods of Measuring Jiigidity.
Torsion of a thin Cylindrical Tube of Circular Section.— The
case of a thin cylindrical tube of circular section tixed at one end and
twisted by a couple whose axis is the axis of the tube, admits of a very
simple solution. We can prove that each cross-section of the tube made
by a plane at right angles to the axis is twisted as a rigid body in its own
plane through an angle proportioned to its distance from the fixed end,
and that there is no displacement of any point in the tube either radially
or longitudinally. The last result follows at once from the symmetry of
the tube about its axis ; for from the symmetry, if the radial displace-
ment is outwards at one part of the section it will be outwards at every
point, so that there would
be a swelling of the tube ;
reversing the couple ap-
plied to the tube would,
however, reverse the dis-
placement (since we sup-
pose Hooke's Law to
hold) ; hence a couple in
one direction would cause
the tube to swell, while
one in the opposite direc-
tion would cause it to
contract ; it is evident,
however, that whether
the tube swells or con-
tracts under a twist about its axis cannot depend upon the direction of the
twist, hence we conclude that there is no radial displacement. Similar
reasoning will show that the longitudinal displacement must also vanish.
We shall now show that the tube will be in equilibrium when each
cross section is twisted as a rigid body through an angle proportional to
the distance of the section from the fixed end.
For suppose ABCDEFGH is a rectangular parallelopiped cut out
of the tube before the twist was applied, suppose the distance between
the planes ABCD, EFGH is d, and let k be the distance of the plane
EFGH from the fixed end of the tube. Then, since the angle through
which each section is twisted is proportional to its distance from the fixed
end, if 0 bo the angle through which the section at unit distance from tho
fixed end is twisted, the rotation of EFGH is A'0, and that of ABCD
is {h->rd) (p. If a is the radius of the tube, and if t, its thickness, is small
compared with a, each point in EFGH will be moved through a distance
Torsion.
19
ak(p, and each point of ABUD through a distance a {k + d) ^, hence
After the twist the shape of the parallelofiiped ABODE FGH will be
dmilar to EFGHA'B'C'D', where A A' = BB' = CO" = DD' = acZf Hence
the deformation of the elements will be a shear of which the angle
of shear = AA'/AE = rt0. The t;ingential stress T will therefore be na(p.
Hence the stresses on the elements will be as shown in Fig. 47,
horizontal tangential stresses equal to T on the faces A BCD, EFGH, and
vertical tangential stresses equal to T on the faces ABEF, ODHG. As 0
is uniform for all parts of the tube these stresses are constant throughout
the tube, and therefore each portion of the interior will be in
equilibrium under these stresses. To find the condition for equilibrium
under the external couple, consider a portion ABOD, Fig. 48, cut from
the tube; this portion is in equilibrium under the action of the tangential
stress T on its cross section, and the external
couple whose moment we shall suppose is C. For
equilibrium the moment of the tangential stresses
round the axis must equal C. The moment of the
tangential stresses is, however, T x area of cross-
section of tube X radius of tube, which is equal to
hence we have C = n(p27raH
(1)
which gives the rate of twist <p when the external
couple is known.
Case of a Solid Rod of Circular Section.—
We can regard the rod as made up of a series of
tubes, and hence from the preceding investigation
we see that each cross-section of the rod will be
twisted as a rigid body through an angle proportional
to its distance from the fixed extremity.* The
couple C required to twist the rod will be the sum of the couples required
to twist the tubes of which it is built up, or in the notation of the
integral calculus,
Fig. 48.
c
ra
= 27r?t^ / r
'dr
nence
if a is the radius of the solid cylinder. If * is the angle through which
the lower extremity of the rod is twisted and I the length of the rod, then
Thus the coiiple_jrequired to^twist the lower ^nd of the bar through a
given angle varies directly as the fourth powerof the radius_and^nversely
as tlie length'oFthe bar. If instead of aTbar we have a thick tube whose
* For if the cross-sections of the different tubes were twisted through different
angles, so as to shear one tube past the next, there would be twisting couples acting
on the inner parts of the tube, and, since the outside of the rod is free, nothing to
balance these on the outside.
80
PROPERTIES OF MATTER.
inner radius is b and outer radius a, the couple (J required to twist its
lower extremity through an angle * is given by the equation
*
G = i7rnj{a'-y]
The work required to twist the cylinder through an angle # can be shown
by a method exactly similar to
tuat given on p. 71 to be equal
to iC* ; hence in the case of a
solid rod the energy is
V
The volume of the rod is Wa-,
hence the mean eneigy stored up
in unit volume of the rod is \na-(i?.
When the cross-section of the
bar is not a circle the problem
becomes much more difficult. It
has, however, been solved by St.
Venantfor a considerable number
of sections of different shapes,
including the ellipse, the equilateral triangle and the square with rounded
corners. In every case except the circle a cross section made by a plan©
at right angles to the axis does not remain a plane after twisting but is
buckled, part of the section l^eing convex and part concave. In these
cases there is a longitudinal displacement of the particles,
some moving up and others down. The longitudinal
movement is the same for all particles that were originally
in a straight line parallel to the axis of the cylinder. We
can see in the following way that there must be longitudinal
displacements of the particles and find the direction of the
displacement. Let us take the case when the section is
an ellipse ; then, if each section were rotated round the
axis without any longitudinal displacement, the stress in
each section at any point P would be at right angles to
the line joining O to that point. Thus, if Fig. 49
represent the section of an elliptic cylinder, twisted in the
direction represented by the arrow, the fixed end of the cylinder being
below the plane of the paper and the twist applied to the end above the
paper, the stress in the section, if there were only rotation, would be at
right angles to OP ; now, if P is a point on the ellipse, the tangent to the
ellipse will not be at right angles to OP except at the extremities of the
axes ; hence in general the stress would have a_component__along the
normaL to the cylinder. Since, however, the sides of the cylinder are
supposed to be free and not acted upon by forces, there cannot be
equilibrium unless the stre.ss along the normal to the cylinder vanishes ;
hence there must be some other displacements which will produce a stress
to balance the normal component of the stress at right angles to OP.
This component is directed outwards in the quadrants AB, A'B', inwards
in the quadrants BA', B'A ; hence the additional stress must be directed
TORSION.
81
inwards in the quadrants AB, A'B', and outwards in the quadrants BA',
B'A. Now suppose PQRSTUVW, Fig. 50, represents a paiallelopiped
cut from the quadrant AB, the faces PQRS, TUVW being at riglit angles
to the axis of the cylinder and the latter nearer to the fixed end, the faces
Y
I *^ If
■•^^ Fig. 52.
PQTU, RSVW being at right angles to" OP ; then there must be a stress
in the plane PQRS directed from R to Q ; but if there is a stress in this
direction there must be a stress in RSVW parallel to RV, otherwise the
parallelepiped would be set in rotation and could not be in equilibrium.
Now the stress in RW parallel to RV implies either that the longitudinal
displacement in the direction RV is greater than that in the same
direction in the face PQTU — i.e., that
the longitudinal displacement increases
as we recede from the axis or else that
the longitudinal displacement in the
opposite direction VR is less than that
in the face TPQU — i.e., that the longi-
tudinal displacement diminishes as we
recede from the axis. But as the
longitudinal displacement vanishes at
the axis itself, it seems clear that it
must increase as we i-ecede from the
axis ; hence we conclude that the
longitudinal displacement is in the
direction RV — i.e., towards the fixed
end of the cylinder. In the quadrant
B'A' the tangential stress at right
angles to OP has a component along Fig. 53.
the outward normal, hence the longi-
tudinal displacement is again towards the fixed end of the cylinder. In
the other quadrants BA', B'A the tangential stress has a component along
the inward normal, and in this case the longitudinal displacement will be
in the opposite direction — i.e., aicay from the fixed end of the cylinder.
Along the axis of the ellipse there is no longitudinal displacement. In
Figs. 51, 52, 53, taken from De St. Venant's paper, the lines of equal
longitudinal displacement are given in Fig. 51, when the cross section of
the cylinder is an ellipse, in Fig. 52, when it is an equilateral triangle,
and in Fig. 53, when it is a square. The dotted lines represent
displacements towards the fixed end of the cylinder, the full lines
displacements away from it. The direction of twist is indicated by the
axrows. It will be seen that in all cases the displacement is towards the
82
PROPERTIES OF MATTER.
fixed end or away from it, according as the component of the tangential
stress at right angles to OP along the normal to the boundary is directed
to the outside or inside of the cylinder. The reason for this we saw
when we considered the elliptic cylinder.
The appearance of cylindeis under considerable twist is shown in
Fig. 54; this case can be realised by twisting a rubber spring of elliptic or rect-
angular section and observing the distortion of lines drawn on the spring.
In the case of the elliptic cylinder, De St. Venant showed that the
longitudinal displacement lo reckoned positive when towards the fixed end
of the cylinder at a point whose co-ordinates referred to the principal
axes of the ellipse are x, y is given by the equation
W = (j)
.«'
b-
a' + b
where a and h are the semi-axes of the ellipse, and ^ the rate of twist,
Fig. 55.
Thus the lines of equal longitudinal displacement are rectangular hyper-
bolas with the axes of the ellipse for asymptotes.
The couple C required to produce a rate of twist ^ was shown by
De St. Venant to be given by the equation
C = ??^7
a^b
3A3
a' + b^
In the case of a thin strip of elliptic section where h is small compared
with a this equation is approximately
C = oiipTrab'
Let us compare this with the couple C required to produce the same
rate of twist in a wire of circular section, the area of the cross-section
being the same as that of the strip. If r is the radius of the cross-sectio?,
then (see p. 79) —h,
60 that
C^^2ab^
TORSION.
8S
Now, as the areas of the cross-sections are the same
vr° = Trab ^
hence
0 ^26
C a
thus, as b is very small compared with a, 0 is small compared with C.
Thus, if we use the torsion to measure small
couples, the strip will be vpry much more
sensitive than the circular wire. Strips of
fhin metal are employed in some delicate
torsion balances.
The greatest strain was shown by De St,
Venant to be in the parts of the boundary
nearest the axis — i.e., the extremities of the
minor axis in the case of the elliptic cylinder
and the middle points of the sides iji the case
of the triangular cylinder.
The stress vanishes at a projecting corner,
as, for example, at angles of the triangle and
square. On the other hand, it becomes
infinite at an internal angle, such as is shown
in Fig. 55. These should, therefore, be
avoided in shafts subject to torsion, or if they
have to be used the angle should be rounded
oft:
Determination of the Rigridity by
Twisting'. — The coeflicient of rigidity n is
frequently determined by means of equation,
(see p. 79) which gives the relation between"
the couple C required to twist a circular rod
of radius a and length I and the angle <I>
through which the rod is twisted by the
couple. The ratio of the couple to the angle
may be determined (1) statically ; (2) dyna-
mically.
In the statical method a known couple is
applied to the wire or rod by an arrangement
such as that shown in Fig. 56, and the angle
through which a pointer or mirror attached to the wire is deflected is
measured. This gives C and $, and if we measure a and I, the preceding
equation gives n.
In the dynamical method for determining the rigidity, the wire whose
rigidity is to be determined hangs vertically, and carries a vibration bar
of known moment of inertia. If this bar is displaced from its position
of equilibrium it vibrates isochronously, and the time of its vibration
can be determined with great accuracy. The torsional couple tending
84 PROPERTIES OF MATTER.
to bring the bar back to its position of equilibrium when it is displaced
through an angle * is equal to
hence, if MK^ is the moment of inertia of the bar, the time T of a complete
vibiation is given by
SkMKH
hence n= ,..,,
J- it
This experiment is easily made and T can be measured very accurately.
The values of n found by this method are, as a rule, higher than those
found by the statical method. Both methods are open to the objection
that, as a occurs to the fourth power, if we make an error of 1 per cent,
in the determination of a the use of the formula will lead to an error of
4 per cent, in the determination of oi. Again, the use of wire in the
determination of elastic constants is objectionable, as the process of wire-
drawing seems to destroy the homogeneity of the metal, the outer layers
differing fi-om the inner. Unless the material is homogeneous it is not
justifiable to use the equation of page 79, and any abnormality in the
outer layers would seriovisly affect the torsion, as it is in these layers that
the strain is greatest. The values of n for all metals are found to decrease
as the tempei^ature increases. (Horton, Froc. Roy. Soc. 73, p. 334.)
CHAPTER VIII.
BENDING OF RODS.
Contents. — Bar bent into a Circular Arc — Energj' in Bar — Bar Loaded at one End —
Depression of End- Bar Loaded in Middle, Ends Tree — Bar Loaded in Middle,
Ends clamped— Vibration of Loaded Bars — Elastic; Curves — .Stability of Loaded
Pillar — Young's Modulus determined by Flexure — Table of Moduli of Elasticity.
By a rod in this chapter we mean a bar of uniform material and cross-
section whose length is great compared with its transverse dimensions.
We shall suppose that such a bar is acted on by two couples, equal and
opposite, applied at the two ends of the rod, the plane of the couples
passing through the centres of gravity of all the cross-sections of the rod,
and intersecting the cross-sections in a line which is an axis of symmetry
of the cross-section. Let the couples act so that the upper part of the bar
is extended while the lower part is compressed. There will, therefore, be
a part of the bar between the top and the bottom which is neither
extended nor compressed. This part of the bar is called the neutral
surfa^, and the section of it by the plane of the couple is called the
neutral axis. Let us suppose the bar divided into thin filaments parallel
Fia. 67.
to its length. We shall now proceed to show that the bar will be in
equilibrium if each filament above tlie neutral surface is extended, each
filament below that surface compressed, the extension or compression
being proportional to the distance of the filament from the neutral
surface, the filaments being extended or compressed as they would be if
the sides of the filament were free from stress ; so that if P is the tension
and e the elongation, V = qe whei^e q is Young's modulus.
First consider the equilibrium of any filament ; the strain is a uni-
form extension or contraction, according as the filament is above or below
the neutral surface. Tlie strain will, therefore, be a uniform longitudinal
tension or compression, there will be no shearing stresses and no stresses \
at right angles to the length of the bar ; all these statements hold whether
the filament abuts on the surface or not. As the only foi'ces acting on
the filament are at right angles to its ends, and are equal and opposite,
the filament will be in equilibrium. Thus each internal portion of the
bar is in equilibrium, and the bar as a whole will be in equilibi'ium if the
stresses due to the strain are in equilibrium with the external forces.
Suppose that the bar is cut at C, and that EFGH (Fig. 58) represents a
cross-section of the bar, 0 being the centre of gravity of the section ; then the
forces acting on the portion OA (Fig. 57) of the bar are the external couple,
86
PROPERTIES OF MATTER.
'iS^QAj-^
whose moment we shall take to be C and the stresses acting across the'
cross section. Thus the condition for equilibrium is that the stresses across
this section should be equivalent to a couple in the plane of bending whose
moment is C, Now the tension acting on the cross-section of a filament
at P is equal per unit area to qe where e is the elongation of the filament.
Now e is proportional to PN if ON is perpendicular to the plane of
bending and PN perpendicular to ON ; let e = aPN. Thus the force acting
on tlie filament parallel to the length of the rod is ^.a.PNw where w is
the cross-section of the filament, and the forces on all the filaments into
which the bar may be supposed to be divided must be together equivalent
to a couple of moment C in the plane of bending. The conditions for this
are (1) that the resultant force should vanish ; (2) that the moment of the
forces about OM, which is perpendicular to ON, should be zero ; and (3)
^ui_ that the moment of the forces about
ON = C. All these conditions can be
fulfilled if OM, ON are the principal
axes of the cross-section.
For the resultant force is S^a.PN.w
where ZqaPN.o) denotes the sum of
the product ga.PN.w for all the fila-
ments ; this vanishes since 2PNw = 0,
0 being the centre of gravity of the cross-
section. The moment of these foi-ces
about OM is equal to E^-aPN.PMw;
this vanishes since SPN.PM = 0, as
OM, ON are principal axes. The mo-
ment of the tension about ON is
25^aPN*w ; this is equal to qaAk- if A^
is the moment of inertia of the cross-
section about ON. Hence the tensions
will be in equilibrium with the external
forces if qaAk' = G.
To find a, let us consider the deformation of a rectangle ABCD (Fig. 59)
in the plane of bending, AB being a portion of the neutral axis. Let
A'B'C'D' be the strained configuration of this rectangle ; then, since there
is no shear, the angles at A' and B' will be right angles, and C'A', D'B'
will be normals to the curve into which the neutral axis is bent ; if these
normals intersect in 0, then O is the centre of curvature of the neutral
axis. We have from the figure
C'D'C'O
A^ ATO
But A'B' = AB, since the neutral axis is not altered in length by the
bending, and AB - CD ;
CD' - CD A'C
Fio. 68.
hence
CD
A'O
But if e is tne elongation along CD, e ■■
CD' - CD
CD
Kence
A'C _ A'C _ AC
' A'O p a
approximately,
BENDING OF RODS.
87
where p is the radius of curvature of the neutral axis at A.
the previous notation e = a.AC, so that a = - •
P
Since qaAk- -» 0, we have q = 0 ; or, p = q — -
P 0
But with
B
Thus the radius of curvatiu-e of the neutral axis is constant, so that the
neutral axis is a circle. '
The fact that a thin bar C\
or lath is bent into a circle
by the application of two
couples is often utilised
for the pur pose of drawing
circles of large radius.
The bending of the ^ ^
bar will be accompanied J
by a change in the shape J
of the cross section. The
elongation of the upper
filaments will be accom-
panied by a lateral con-
traction equal to a times
the elongation where a is
Poisson's ratio (see p. 73),
while the shortening of
the lower filaments will
beaccompaniedbyalateral Fio. 59.
expansion. Thus the
shape of the cross-section supposed to be originally a rectangle will after
the bending be as represented in PQLM (Fig. 60).
Suppose LM is the line where the neutral surface cuts the cross
section, then the lateral contraction of PQ is equal to
LM - PQ
LM
and the longitudinal extension is equal to
P
LM - PQ QM . , . ,
hence — ^ ^r — ^ ^ ■' -
LM p
but if LP, MQ intersect in O', then ^^^"^^ = ^
^^""^ Tw --
.r
But LO' is equal to the radius of curvature of the neutral surface in
the plane at right angles to the length of the rod. If this is denoted by
p' we have
<rp' = p
Thus the ratio of the two curvatures is equal to Poisson's ratio.
88
PROPERTIES OF MATTER.
Energy in the Bar. — Consider one of the filaments into which the
bar was supposed (p. 85) to be divided. Thus, if e is the elongation in
this filament, I the length of the filament (which is equal to the length of
the bar), w the area of its cross-section, the energy in the filament is by
p. 71,
Iqe
^U.
But e = a.PN;
hence the energy in the filament is J^a-PN-w?.
The energy in the bar is the sum of the
energies in tlie filaments, and is thus
^qaH-LVWut ; but SPN^w = Ak\
and a = l/p where p is the radius of curva-
ture of the natural axis, and thus the
energy is equal to ^qAkH/p-.
Again, qaAk" = C, where 0 is the couple
applied to the bar,
hence the energy = |C-
P_
= half the product of the couple and
the angle between the tangents at the
^ extremity of the bar. This result could
be deduced at once by the method already
given.
Rod bent by a Weigrht applied at one End.— In the case just
FiQ. 60.
I*
Fia 61.
considei'ed the stresses in the bar were entirely normal ; in this case, how-
ever, we see that for equilibrium the normal stresses must be accompanied
by tangential ones. For, suppose ACB, Fig. 61, represents the bar, the
weight being applied at B while A is fixed ; consider a section through C
made by a plane at right angles to the length of the bar. Then the
portion CB of the bar must be in equilibrium under the action of the
stresses across the section at C and the weight W at the end of the bar ;
thus the stresses across C must be equivalent to a vertically upward force
BENDING OF RODS.
89
W and a couple whose moment is W.BC : there must be, therefore, tangential
stresses acting across the section whose resultant is a force W acting
upwards. We shall show, however, that if the lateral dimensions of the
bar are very small, then, except quite close to the end 15, the tangential
stresses will be very small compared with the normal stresses. For let
EFGH represent a section of the bar, O the centre of the section, and ON
an axis at, right angles to the plane of bending. Then, if A is the area of
the cioss-section, T the average tangential stress over the area
TA = W
Let N represent the normal stress at a point P, dw a small area round P,
then since these normal
stresses are equivalent to a ^ -^
couple whose moment round
ON is W.BC, we have
/
N.PN(Zw = W.BO.
Thus the average normal 0
stress must be of the order
of magnitude
W.BO
Ad
^
Fig. 62.
where c? is a quantity comparable with the depth of the bar. Hence,
W
since — = T, the magnitude of N is comparable with T x BO/tZ, so that if the
distance of the section from the end is large compared with the lateral
dimensions of the bar, the normal stresses will be very large compared
with the tangential ones. In the subsequent work we shall confine our
attention to the effect of the normal stresses, but this must be regarded as
an approximation only applicable to very thin rods. Let Fig. 62
represent a small rectangular parallelopiped cut out of the bar, the faces
EFGH, E'F'G'H' being at right angles to the length of the bar, while the
faces FF'H'H, EE'GG' are parallel to the plane of bending, then the
actual state of stress may be thus described. The normal stresses are
confined to the faces EFGH, E'F'G'H', there being no normal stresses
over the other faces ; there are tangential stresses on the faces FF'HH',
EE'GG', and also on the faces GG'HH' and EE'FF', but there are no
tangential stresses over the faces EFGH, E'F'G'H'.
We may proceed to find the bending of the rod produced by the
weight at its end in the following way. Suppose PQRS (Fig. 62a) represents
a portion of a rod bent as on p. 85, by couples of moment C acting at its
ends, then the stresses in the bar are such as to cause a couple with
moment C to act across PQ and a couple whose moment is C to act across
the section ES. The stresses which produce these couples, as we have
seen on p. 87, coirespond to a state of strain such that the central axis of
the portion of the bar is bent into a circle whose radius p is given by the
equation
q—=0.
9
90
PROPERTIES OF MATTER.
Now suppose that PQRS, instead of being a portion of a bar acted on
by a couple, is a portion of one acted on by a force at the end A : then
ne^^lectin", for the reasons given above, the tangential stresses across the
sec°tion, the stresses are equivalent to a couple W. AN across the section PQ
and a couple W.AM across the section US, and as AN and AM differ but
little from AL whei^e L is
/' // ,
N\ L \M-
Fia. C2a.
the middle point of MN,
we may regard the ends ,
of PQRS as being acted,
on by equal and opposite '
couples whose moment is
W AL. Hence, by what we have just seen, the central axis of PQRS will be
bent into the arc of a circle whose radius p is given by the equation
g.^ = W.AL;
hence when thej)ar is^ac^ted jnijjy^aweight ajaplied at one end, the neutral
'^s^'the^bar is bent into a curve such that the radius of curvature at a
^Hnl.'v^rles ihvei-seTy^agjfche_clistah^ of ;the_^oint from the^nd to which
the weigTiFisli^plied. ^ .. ^
Depression of the Bar; Ang-le between Tangfents at two
Points on the neutral Axis.— Suppose Pig. 63 represents the curved
Fig. 68.
position of the neutral axis.* Suppo.se RS are two points near together
on the neutral axis, then the angle between the tangents at R and S is
equal to RS/p where p is the radius of curvature of RS ; but 1/p is equal
to W.Altxjq.Ak-, hence Ao the angle between the tangents at R and S is
equal to
W
q.A/c
AR.RS
* Though this figure shows for clearness' sake considerable curvature, yet it must
be remembered that in all these investigations we are only dealing with cases in
which the bending is very slight and the neutral axis consequently nearly straight.
BENDING OF RODS. gi
or, in the notation of the differential calculus, if s — AR, we have
^^=,^> (1)
hence S, the angle between the tangents at A and P, is given by the
equation
a
= i-~ AP2
Suppose the tangent at P cuts the vertical through A in the point T,
we shall proceed to find an expression for AT. Let the tangents at K,S
cut the vertical line through A in the points ;M,N, then, remembering that
these tangents are veiy nearly horizontal, we have approximately, if Ao is
the angle between the tangents at R and S,
MN = AR.A6=^-f c/a by (1)
AP
J oAk' 8 X a Alt' ^ '
NowAT = .MN^^^^,_. ^^^^^
If the end B of the bar is clamped so that the tangent is horizontal,
then the distance between A and the point where the vertical through A
cuts this tangent will be the vertical depression of A produced by the
weight W ; hence, if d be this depression, we have by (3)
z*^- \ d = --^,-A^' (4)
yQ.\>Y^i5iof^- 1^^215:
Thus the vertical depression of the end is proportional to the weight,
to the cube of the length, and inversely proportional to the moment of
inertia of the cross section about an axis through its centre at right angles
to the plane of bending ; it is also inversely proportional to the value of
Young's modulus for the material of which the bar is made.
Since the depression is proportional to the weight, the energy stored
in the bar is equal ^Wd, and this by equation (4) is equal to
We shall now proceed to find the depression PM (Fig. 64) of any point
P on the bar below the horizontal tangent at B. Let the tangent to the
central axis at P cut the vertical line through A in the point T, and let the
horizontal line through P cut this line at O ; then the vertical depression
of Pis
PM = AN-AT-TO
Now TO = PO X angle the tangent at P makes with the tangent at
B, and since PO is approximately equal to AP, and the tangent at A
makes with the tangents at P and B angles whose circular measures are
92
PROPERTIES OF MATTER.
respectively W.A'Py^qAk' and W.AB72^A^^ (by equation (2)), we
have
AP W
TO = ^^ iJ2_(aB- - AP=)
2qAk- '
By equation (3) we have
Thus
Hence
AN = — ^ AB»
3^AP
W
AT-^ , AP-^
3gA/fc-
FiG. 64.
PM- ^ rAB«-AP3_AP(AB^-AP0^ ^ .^.. ^.m-
?AF\ 3 2 / ^1
W BP-r3AP + 2BP)
\ 6
qkJi
I
- t
:t fAf--'rr/^.-i^^Os
(f)
f/^/'^
^- fJP'f
Fig. G5.
Let us now find what would be the depression of A if the weight W
were applied at P. In this case AP would be straight, and if AN,
Fig. 65, is the depression of A,
AN = PM + AP X angle which tangent at P makes with the horizoctal
Now by (4)
W
PM = :^,BF
and by (2) the angle the tangent at P makes with the horizontal i;
equal to
W
2qAk'
BP^
hence
BENDING OF RODS.
qAk^ I 3 +-2"j
= _^BP^' f3AP+2BP
93
}
(6)
Comparing equations (5) and (6) we see that the depression at P_when Jha
loa4_js^ap£lied__atjL Jsjbjie_same^^ at A when the load is
applied^^^ In the case we have just been considering one of the points^
IS at the end' of the rod. The theorem, however, is a general one and
holds wherever the points A and P may be. '
The relation between the depression and the weight given by equa-
tion (4) gives us a means of determining q by measuring the flexure of
a beam. In experiments made with this object, however, it has been
more usual to use the system considered in the next paragraph, that of a
beam supported at the ends and loaded in the middle.
Beam Supported at the Ends and Loaded in the Middle.— The
ends of the beam (Fig. 66) are supposed to rest on knife edges in the same
horizontal line. The tangent at 0, the middle point, is evidently hori-
zontal, and the pressure on each of the supports is W/2. Considering now
the portion AC of the rod, it has the tangent at C horizontal, and it is acted
upon by a vertical force equal to W/2 at A. The conditions are the same
as for a rod of length AC clamped at C and acted on by a vertical force
W/2, the case just treated ; hence by equation (4) d, the vertical distance
between A and 0, is given by the equation
d:
3)^t»^& S&l OVi.
W AC^
'IqKk' 3
w
A^Kk""
K&
Rod Clamped at both Ends and Loaded in the Middle.—
Suppose AB is a rod loaded at C, its middle point, and clamped at the
ends A and B, which are supposed to be in the same horizontal line.
^
94 PROPERTIES OF MATTER.
The action of the supports A, B on the rod will be equivalent to a vertical
force and a couple. The magnitude of the vertical force is evidently W/2 if
W is the weight at C. We can find the value of the couple r as follows .
By the action of the force W/2 alone the tangent to the neutral
axis at A would make, with the tangent at 0, an angle whose circular
measure is
W AC^
2yA^- 2
But since the tangent at A is parallel to the tangent at C, the couple
must bend the bar so that if it acted alone the tangent at A would make with
that at C an angle equal and opposite to that just found. Through a couple
r applied to the bar the tangents at A and C wovdd make with each other
an angle whose circular measure is p-
hence
or
To find the depression of the middle point, we consider the efiect of the
foi"C" W/2, and the couple r separately. In consequence of the action
of the force W/2, the middle point, 0 would by equation (4) be depressed
below the line AB by
W AC3
The couple r would bend the bar into a circle whose radius p is qAk^Jr.
This would raise the point C above A by
AC2 -i
r
qAk-
AC
f
W AC=
2qAk' 2
r
qAk^
AO
r=i
W.AC.
• ,^rw
2p
. , rAC-_ W AC»
*-^-' ^ 2p:f~2^aFT~ *' ^
The depression of C when both the force and the couple act is therefore
W AC^ _ W AC^
2qA/c' ~Y~ 'JqAk' T
- W _^ WAB' (
24qAk- U)iVyA^-) D e \5 V' e- 3 3 ) 0 n.
The depression^of the middle point of the bar when the ends are fixed is
thus only l^Tof the depression ot the same bar when the encls7\re free —
""Vibration of Loaded Bars.— Since the deflection of the bar is in all
cases proportional to the deflecting weight, a bar when loaded will execute
isochronous vibrations, the time of a complete vibration being equal to
where M is the mass of the load and ^ the force required to produce unit
BENDING OF RODS.
95
depression. From the preceding investigations we see that fi=p.qkh-IP
where I is the length of the bar and p a numerical factor, which is equal
to S when the weight is applied at the end of the bar, to 48 when the
weight is applied at the middle point of a bar with its ends free, and to
192 when the load is applied to the middle point of a bar with its ends
clamped.
To take a numerical example. Let us suppose we have a steel bar
30 cm. long, 2 cm. bioad, and "2 cm. deep, loaded at the end with a mass
of 100 grammes. Then since for steel 3^ = 2-139 x 10'^, and in this case
M = 100, p = 3, Z = 30, A = -4, h- = \ (•1)==0033, we find by substituting
in the formula that the time of vibration is about \ of a second.
To take another case, suppose a man weighing 70 kilogrammes stands
on the middle of a wooden plank 4 metres long, 30 cm. wide, and 4 deep,
supported at its ends, what will be the time of swing ? For wood we may
take 17 = 10"; putting ;> = 48, M-7xl0\ ^ = 4 x 10^ A = 120, h? = \{2y
= 1'33, we find that the time of swing is about '5 seconds.
A^
B
FlQ. 68.
'^ Elastic Curve. — Let us now consider a case like that of a bow
where the force is parallel to the line joining the ends of the bar. Con-
sider the equilibrium of the portion CB (Fig. 68) under the stresses at C,
and the tension T in the string at B.
Thus the stresses across C must be equivalent to a couple T.CN and a
force T, CN being the perpendicular from C on the line of action of the
force. Confining our attention to the couple, we see that if p is the radius
of curvatures at 0 of the neutral axis of the rod,
^:^=T.CN
(1)
where q is Young's modulus for the rod, A^^, the moment of inertia of
the cross-section of the rod about an axis through its centre at right
angles to the plane of bending. From equation (7) we see that 1/p is propor-
tional to CIST; hence the curve into which the central axis is bent is such
Fig. 69.
96
PROPERTIES OF MATTER.
that th« reciprocal of the radius of curvature at any poii:.t \s proportioual
to the distance of the point from a straight line. Curves having this
property are called elastic curves or elasticas ; curves such as those shown
in Fig. 69 are included in this family ; they may be produced by taking
a flexible metal ribbon, such as a watch-spring, and pushing the ends
too-ether. One of these curves is of especial importance — ^viz., the one
where the distance of any point on the bent rod from the line of action of
the force is very small. We shall show that this curve is tlie path of a
point near the centre of a circle when the circle rolls on a straight line.
To prove this it is only necessary to show that the reciprocal of the radius
of curvature of this path is proportional to the distance from the straight
line which is the path of the centre of the circle. Let us suppose that the
circle rolls with uniform angular velocity w along the straight line. JUit
C be the centre of the circle, P any position of the moving point, G the
point of contact of the circle with the line along which it rolls, PN the
perpendicular on GO. Then if v be the velocity of the point, p the radius
of curvatui-e of the path,
— = acceleration of P along the normal to its path (8)
p
Now sinco the circle rolls on the line without slipping the velocity of G is
zero. Hence the system is turning about
"^^^ -^ ~"^ G, so that the velocity at P is at right
angles to PG and equal to wPG ;!
hence PG is the normal to the path
and
v = w.PG. ^
Now the acceleration of P is equal to
the acceleration of 0 plus the accelera-
tion of P relative to 0 ; since 0 moves
uniformly along a straight line the
'acceleration of 0 is zero, and since P
describes a circle round 0, the accelera-
tion of P relative to C is equal to w^GP
and is along PC. Thus the acceleration of P along the normal to its path
is equal to
and we have therefore by (8)
w'CPcosCPG
iii
=^PG2
= w-CPcosCPG
or
l^CPcosCPG
P
PG^
Since the angle PGC is very small, the angle CPG is very nearly equal to
the angle PCN, and PG is very nearly equal to «, the radius of the rolling
circle ; hence approximately
l^CPcosPON
a-
CN
a'
BENDING OF RODS.
97
Thus l/p is proportional to the distance of P from the straight line
described by 0.
From the equation
we see that
a
"T~
The shape of the curve is shown in Fig. 71. The distance between
two points of inflection, that is, between two points, such as A and B, ^
where Ifp vanishes, is equal to ira.
Stability of a loaded Pillar.— The preceding result at once gives
us the condition that a vertical pillar with one end fixed vertically in the
ground should not bend when loaded with a weight W — i.e., the condition
that the pillar should be stable. For, suppose the pillar bends slightly,
assuming the position AB, Fig. 72, then AB is an elasticaand B must be a
point of inflection, while, since A is fixed vertically in the ground, the tangent
at A is parallel to the line of action of the force. The distance — measured
parallel to the base-lines — between a point of inflec-
tion and the point where the tangent is parallel to B
the base-line is half the distance between two points
of inflection, and is, therefore, equal to ^ttcs, or, sub-
stituting the value of a, to
V ^
where W is the weight ; hence, in order that the
pillar should be able to bend, I, the length of the
pillar, must not be less than
^ W
or, in order to avoid bending,
W
w
w
(9)
If the cross-section of the pillar is a circle of
Thus the weight which a
■irW
Fig. 72.
i-adius 6, then AJc' = ^ivb^,
vertical pillar can support without becoming unstable
IS proportionaLtojthe fourth power of the radius and
inversely proportional to the_sc[uare of the length of the pillar^ To take
ar"special case, let us consider a steel knitting-needle, 20 cm. long and
•1 cm. in radius and take q = 2-U x 10^^ We find W less than 1-04 x 10"
- — i.e., less than about 1056 grammes.
If the rod, instead of being fixed at one end, is pressed between two
G
/<r^
98
PROPERTIES OF MATTER.
supports so that the ends are free to bend in any direction, Fig. 73, the
ends must be points of inflection, the distance between which is -na or
hence
KsJqAk'/Wl
in the limiting case when the pillar can bend. Hence for stability
W<
(10)
In the case where both ends are fixed (as in Fig. 74), the tangents at
B B
Fig. 73.
Fig. 74.
the ends must be parallel to the line of action of the force, and there must
be two points of inflection at, 6andc; hence the distance between the ends
is twice the distance between two points of inflection, so that
l=2iva
9 fq^h;'
Hence for stability
w.
-q£
AA^
(11)
Comparing (9) and (11), we see that a rod with both ends fixed will,
without buckling, support a weight sixteen times greater than if one end
were free.
Since a pillar can only support without buckling a finite weight, and as
this weight diminishes as the length of the pillar increases, it follows that
a pole of given cro.ss-section would, if high enough, begin to bend under its
owu weight, so that there is a limit to the height of a vertical pillar or
BENDING OF RODS. 99
tree of given cross-section. Suppose VV is the weight of the pillar, and
suppose as an approximation that the problem is the same as if the weight
were applied at the middle point of the pillar, then if I is the length of
the pillar we see from (9) that
I'
or
A more accurate investigation, which requires the aid of higher
mathematics, shows that the accurate relation is
Let us take the case of a pine tree of uniform circiilar section from top to
bottom, let the diameter of the tree be 15 cm. For deal g'=10", and
taking the specific gravity of deal as '6, we have
„ 7-84 X 10" X 15^
^e get "<—7. — 7rT\ — T7, —
^ -6x981x16
;<2 7xl0'cm.
Thus the height of the tree cannot exceed about 27 metres.
Determination of Young-'s Modulus by Flexure. — Young's
modulus is often determined by measuring the deflection of a beam supported
at both ends and loaded in the middle. If d is the depression of the middle
of the bar, then (see p. 93)
d = — ^_ AB'
48<7Ay5;-
where W is the load, AB the length of the bar, q Young's modulus, Ak''
the moment of inertia of the cross-section of the bar about an axis through
the centre of gravity of the section at right angles to the plane of bending.
The value of d can be determined by fixing a needle point to the middle
of the bar, and observing through a microscope provided with a micrometer
eyepiece the depression of the beam when loaded in the middle with various
weights. Another method of measuring d is by means of a very carefully
made screw, the end of which is brought into contact with the bar; by
measuring the fraction of a turn through which the head of the screw-
must be turned to renew the contact after the bar has been loaded we can
determine the value of d corresponding to given loads. The most accurate
method, how^ever, would be an optical one, in which, by Michelson's method,
interference fringes are produced by the interference of light reflected
from two mirrors, one of which is fixed while the other is attached to the
middle point of the bar. By measuring the displacement of the fringes
when the load is put on we could determine d, and the method is so
delicate that the displacenaents corresponding to very small loads gould b©
100
PROPERTIES OF MATTER.
Another method, due to Konig, consists in measuring the angle through
which the free ends of the bar are bent. The method is represented in
Fig. 75. AB is the rod resting on two steel knife edges S,, S,. The mirrors
Pp P,, which are almost at right angles to the rods, are rigidly attached to
it. The vertical scale S is reflected first from the mirror P^, then from
the mirror Pj, and then read through the telescope F. The Aveight is
applied to the knife edge r, which is exactly midway between the knife
edges Sp S^. On looking tlii'ough the telescope we find one of the divisions
of the scale coinciding with the cross wires; on loading the beam another
division of the scale will come on the cross wire, and by measuring the
distance between these divisions we can determine the angle ^> through
which each free extremity of the bar has been bent. For, let us follow
n
Fig. 75.
the ray backward from the telescope ; when tlio minor P, is twist<^d
through an angle ^, the point where the reflected ray strikes the mirror
P, is shifted through a distance 2cZ0, where d is the distance between the
mirrors; thus, if the light reflected from P, were parallel to its original
direction, the scale reading would be altered by 2d(f>, but the light reflected
from Pg is turned through an angle 40 ; this alters the scale reading by
4D0 where D is the distance of the scale S from the mirror P^j, hence v, the
total alteration in the scale reading, is given by
'v = {-ld + \J))(p
Tluis
but. (see p. 91)
^ 2d + 4D
W P
f =
2.qAk' 8
where I is the distance between the knife-edges.
Thus knowing v we can determine q. The advantage of this method is
that V, the alteration in the scixle reading, may be made very much greater
than the depression of the middle of the bar.
BENDING OF RODS.
101
The following cotiveniont method for cletLTiniuiug hoth a ;iiul q for ;i
wire was given by G. F. 0. Searle in the Philosophical Matjazine, Feb. IDOO.
AB, CD (Fig. 7()) are two e<pial bras.s bars of square section, the wire
under observation is lirnily secured by passing throiigli horizontal holes
drilled through the centres G, G' of the bars. The system can be suspended
by two pai-allel torsionless strings
by means of hooks attached to the
bars. If now the ends B and D
are made to approach each other
through equal distances and are
then set free the bars will vibrate
in a horizontal plane. To a tirst
approximation the centres G and G'
remain at rest, so that the action
of the wire on the bar, and therefore
of the bar on the wire, is a pure
couple ; the wire will, therefore, be
bent into a horizontal circle and
the couple will be qA^k-jp. Here
q is Young's modulus, Ak- the
moment of inertia of the cross-
section of the wire about an axis
through the centre of gravity at
right angles to the plane of bending,
p the radius of curvature of the
wire, which is equal to 1/2(1} if I is the length of the wire and (p the angle
through which each bar is twisted. Hence, is K if the moment of inertia
of CD about a vertical axis through G, we have
Fio. 76,
^d'(t> qAk- 2(7 AF
de
I
hence, if T, is the time of vibration,
T =9^ /J5
Kl
.qAk'
(12)
The bars are now unhooked from the strings and one clamped co a shelf,
so that the wire is vertical ; if we make the wire execute torsional vibra
tions, and T, is the time of vibration,
V 7r?ia
(13)
(see p. 84), n being the coefficient of rigidity and a the radius of ice wire
As the wire is of circular section,
hence by (12) and (13) we have
Ak' = '^;
n T,«
102
PROPERTIES OF MATTER.
TABLE OF MODULI OF ELASTICITY.
The values of the moduli of elasticity vary so much with the treatment a meta
has received in wire-drawing, rolling, annealing, and so on, that whenever thej
are required ior a given specimen it is necessary to determine them, if any degree
of accuracy is required. The following table contains the limits within which
determinations of the moduli of different metals lie. They are taken from the
results of experiments by Wertheim, Kiewiet, Lord Kelvin, Pisati, Baumeister,
Mallock, Cornu, Everett, and Katzenelsohn. The values are given in C.G.S. units,
n is the rigidity, q Young's modulus, k the bulk modulus, and <t Poissou's ratio.
%
cr-
3 K-3-n
nAO"
g/ion
A/IO"
<r
Aluminium ,
2-38— 3 -36
7-4
-13
Brass .
3-44— 4-03
9-48- 10-75
10-2- 10-85
•226— -469
Copper .
3-5— 4-5
10-3— 12-8
17
•25 — -35
Delta-Metal .
3-6
9-1
10
—
Glass .
1-2- 2-4
5-4- 7-8
3-4-4-2
-20— -26
Gold .
3-9— 4-2
f 5 -48 (drawn))
\ 8 (rolled) /
—
•17
Iron (cast) .
3-5- 5-3
9-8—16
9-7—14-7
•23— ^31
Iron (wrought)
6 -6-7 -7
17—20
—
—
Lead .
•18
•5-1-8
3-7
•375
Phosphor Bronze .
3-6
9-8
—
—
Platinum
6-6~7-4
15 17
—
•16
Silver .
2-5— 2-6
7-0— 7-5
•37
Steel
7-7— 9-8
18—29
14-7-19
•25— ^33
Tin
1-5
4-2
Zinc
3-8
8-7
—
•20
CHAPTER IX.
SPIRAL SPRINGS.
Contents. — Flat Springs — Inclined Springs — Angular deflexion of Free End
on Loading — Vibrations of Loaded Spring.
^,
The theories of bending and twisting have very important applications
to the case of spiral springs. By a spiral spring we mean a uniform wire
or ribbon wound round a circular cylinder in such a way that the axis or
the wire makes a constant angle with the generating lines of the cylinder.
The first case we shall consider is that of a spiral spring
made of uniform wire of circular cross-section, and wound
round the cylinder so that the plane of the wire is everywhere
approximately perpendicular to the axis of the^ylinder — i.e., a
"tlat" spring. Let us suppose that such a spring is hung
with its axis vertical, and that a weight W, acting along the
axis of the cylinder, is applied to an arm attached to the
lower end of the spring.
Considering the equilibrium of the portion CP of the
spring, the stresses over the cross- section P must be in equili-
biium with the force W at C, and hence these stresses must
be equivalent to a tangential force W acting upwards, and a
couple whose moment is Wa and whose axis coincides with the I
axis of the wire at P, a being the radius of the cylinder on
which the axis of the wire lies. If the diameter of the wire is
very small compared with a we may, by the principles ex-
plained on p. 89, neglect the effects of the tangential force in
!comparison with that of the couple and consider the couple
alone. This couple is a toi-sional couple and is constant all
along the wire ; it will produce, therefore, a uniform rate of
twist ; if ^ is the rate of twist, b the radius of the wire, and
n its coefficient of rigidity, then we have (see p. 79),
Wa = |7rw6*0.
Now suppose that we have a series of arms of length a
attached to the wire at right angles, the free ends of these
arms all being in the axis of the cylinder. Then, if P, Q are
two points near together, the effect of the twisting is to
increase the vertical distance between the ends of the arms
attached to P, Q respectively by PQ x af, and since a and ^ are constants |
this result will hold whatever the distance between P and Q. Suppose Q is at
the fixed and P at the free end of the spring, then the increase in the
vertical distance between the arm attached to P and Q will be the vertical
depression of the weight W ; in this case PQ = /, the length of wire in the
spring
W
Fig.
^
hence, if d is the depression of W,
Vs
s'-
104 PROPERTIES OF MATTEB
:P^i^
d=l xaxf
Thus d varies directly as the area of the cross-section of the cylinder
and inversely as the square of the area of the cross-section of the wire. We
see that the depression of the weiglit is the same as the displacement of
the extremity of a horizontal arm of length a attached to the end of the
Y same length of wire when pulled out straight and hung vertically, the end
, of the horizontal arm being acted on by a horizontal force equal to W at
aU'^. right angles to the arm.
' To take a numerical example : suppose we have a steel spring 300 cm.
long wound on a cylinder 3 cm. in diameter, the diameter of the wire
being '2 cm.
w = 8xl0", a = l-5, b = -l.
If this spring is loaded with a kilogramme so that W = 981 x 10^, the
depression d will be given by
^_600x981xl0^x(l-5)'
7rx8x lO'^xlO-*
= 5 cm. approximately.
Energry in the Spring". — Q, the energy stored in the spring, is
(see p. 80) given by the equation
Q = iTrnlby
2Wa
But ^ =
thus Q
Trnb*
Trnb*
This result illustrates the theorem proved on p. 71.
Spring-s inclined at a finite Ang-le to the horizontal Plane.—
The flat spring, as we have just seen, acts entirely by torsion ; in inclined
springs however, bending as well as torsion comes into play. Let the axis of
the spring make a constant angle a with the horizontal. Let the spring
(Fig. 78) be stretched by a weight "W acting along the axis of the cylinder
on which the spring is wound. Then, considering the equilibrium of the
portion AP of the spring, and neglecting as before the tangential stresses
at P, we see that the stresses at P must be equivalent to a couple whose
moment is Wa, and whose axis is PT, the horizontal tangent to the
cylinder at P. This couple may be resolved into two : — one with the
moment \V«cosa and axis along the wire PQ, tending to twist the spring ;
the second, having the moment Wasina and its axis PN at right angles to
the plane of the spring at P tending only to bend the spring. Now the
twisting couple Wacosa will produce a rate of twist <p given by
_ Wacosa
SPIRAL SPRINGS.
105
/\
\)
where C is a quantity depending on the shape and size of the cross-
feection of the spring. When the spring is a circular wire of radius 6, we
have seen that C = 77672. The couple Wasina will bend the spring and
will alter the inclination of the tangents at two neighbouring points PQ by
Wa^ino . PQ
^^T-^
where D = A^*, the moment of inertia of the area of the cross-section
of the wire of the spi'ing about an axis through
its centre of gravity at right angles to the plane
of bending.
Let us now
changes on the radial arms
spi'ing-
consider the effect of these
which we imagine
fixed to the spi-ing. Let us first consider the
vertical displacements of the ends of the arms at
two neighbouring points PQ. Taking first the
torsion, the relative motion of the ends is PQ^a,
but in consequence of the inclination of the
spring this relative motion is inclined at an
angle a with the vertical so that the relative
vertical motion is
PQ.Wa''cos''a
PQfwpcosa = p
Thus, if I be the length of the wire in the
spring, the vertical displacement of the end of
the spring due to torsion is
ZWa^cos^a
Now consider the effect of the bending on the
vertical motion of the ends of the rods at PQ.
In consequence of the bending, the relative
motion is in a plane making an angle a with the
horizontal plane and is equal to
Wasina
qD
PQa
L<-^--
«.*>■
To get the vertical component of this we must multiply by sina, and
we see that the vertical displacement due to bending is
PQ
Wa-sin'^a
or for the whole spring
qj)
IWa-sin^a
—qB
Thus the total vertical displacement is
^fcos-a
i.-J
Y^^i" * c a
3) > S^<^ld'=ev^^G
i
ma-
i nG
sin^a\
106 PROPERTIES OF MATTER.
In addition to the vertical displacement there will be an angular dis-
placement of the pointer at the end of the bar which we may calculate as
follows. First take the torsion. The arm at Pis twisted relatively to the
arm at Q through an angle in a plane making an angle - - a with the
horizontal plane equal to PQ x f ; the angular motion in the horizontal
plane is, therefore,
PQ X ^ X cos I ^ - a I
or p^WasinacoPa
And the direction is such that as we proceed along the spring the arms are
rotated in the direction in which the spring is wound, so that this angular
movement due to the toi-sion is such as to tend to coil up the spring.
The angular deflection due to torsion for the whole spring is, therefore,
^.Wasinacosa
Let us now consider the angular deflection due to bending. The arm at
P is bent relatively to that at Q through an angle
.Wasina
PQ-
q\y
in a plane making an angle a with the horizontal plane ; projecting this
angle on the horizontal plane the relative angular motion in this plane of
the two arms is
p^. Wasinacosa .
^ qD *
thus the angular deflection due to bending for the whole length of the
spring is
iWosinacosa
" qiy
The deflection in this case is in the opposite dii'ection to that due to the
torsion, and is such as to tend to uncoil the spring. The total angular
deflection is thus
H.^rixovv-t^i lAV«sinacosa|-i-i-^
in the dii-ection tending to coil up the spring. The angular deflection is
thus proportional to sin a cos a and is greatest when a = 3r/4. The deflection
tends to coil up the spring or uncoil it according as
if the spring is very stifi'to resist bending in its own plane, it will coil up
under the action of the weight ; if, on the other hand, it is very stiff to
resist torsion, it will uncoil. This is exemplified by the two springs
shown in Figs. 79, 80. The first, which is made of strip metal, with the shon''
SPIRAL SPRINGS.
107
dimension in the plane of bending, is very weak to resist bending, and so
tends to uncoil when stretched, while the second, which is also made of a
strip of metal, but with the long side in the plane of bending, is very stiff
to resist bending, and so tends to
coil up when stretched. In the
case of a circular wire of radius h
C:
hh^
so that
1- 1
«C qT>
For metals q is greater than 2?i, so
that
L-i.
?lU qD
is positive, and thus a spring made
up
tends to coil
^V
of circular wire
when extended.
Vibrations of a Loaded
Spring". — We can use the up and
down oscillations of a fiat spiial
spring to determine the coefficient
of rigidity of the substance of which
the spring is made. Let us take
the case of a fiat spiral spring made
of wire of circular cross-section ;
then, if the spring is extended a
distance x from its position of equi-
librium, the potential energy in the
spring is (see p. 104) equal to
X- (1)
/
TT?
Ud"
where n is the coefficient of rigidity,
h the radius of cross-section of the 'I I
wire, a the radius of the cylinder ^^^- 79- Fig. 8Q
on which the spring is wound, and
I the length of the spring. If the end of the spring is loaded with a mass
M, the kinetic energy of this mass is equal to
'dx\
di
IM
The spring itself is moving up and down, so that there will be some kinetic
energy due to the motion of the spring. To a first approximation the
vertical motion of a point on the spring is proportional to its distance from
the fixed eud, so that the velocity at a distance s from the fixed end will be
s dx
108 PROPERTIES OP MATTER.
If p is the mass of unit length of the spring, the mass of au element of
length ds is pds and its kinetic energy is
, /dxVs'
''[dt! r^'
fntegrating this expression from s = o to s = Z, we find that the kinetic
energy of the spring is
^dt
or if m he the mass of the spring
H\dt)
hence the total kinetic energy is equal to
Since the sum of the kinetic and potential energy is constant
\ 3j\dtJ Ua^
is constant, hence differentiating with respect to t we have
This equation represents a periodic motion, the time T of a complete
vihration being given by the equation
T = 2^A/M+m73
^ ivnb'ma'
When T has been determined n can be found by this equation.
Angular Oscillations.* — We can prove in a similar way that T,
the time of vibration of a suspended bar about the vertical axis, is given
by the equation
where MP is the moment of inertia of the bar about the vertical axis and
q Young's modulus for the wire, by measuring T, we can determine q.
* Avrton and Ferrv. Proc. R.S., vol. xxxvi,, p. 311 ; Wilbeiforce, Pliil. Mag.,
Oct. 1894.
CHAPTER X.
IMPACT.
Contents. — Co-efficient of Restitution — Newton's Experiments — Hodgkinson'g
Experiments — Example of Collision of Kaihvay Carriages — Hertz's Investiga-
tions— Table of Coefficients.
Co-efficient of Restitution.— An interesting class of phenomena
depending on the elasticity of matter is that of collision between elastic
bodies. The laws governing these collisions were investigated by Newton
and his contemporaries, who nsed the following method. The colliding
bodies were spherical balls suspended by strings in the way shown in
Fig. 81 ; the balls, after falling from given heights, struck against
each other at the lowest point, and after rebounding again reached a
certain height. By measuring these heights (and allowing, as Newton
did, for the resistance of the aii) the velocities of the balls before and
after collision can be determined. New-
ton in this way showed that when the
collision was direct — i.e., when the rela-
tive velocities of the two bodies at the
instant of collision was along the common
normal at the point of impact — the
relative velocity after impact bore a
constant ratio to the relative velocity
before impact — the relative velocity
being, of course, reversed in direction.
Thus, if u, V are the velocities of the
bodies before impact, u being the velocity
of the more slowly moving body, while ,
U, V are the velocities after impact, i
then
U-V = e(v-M) (1)
,- - , Fig. 81.
where e is a quantity called the co-
efficient of restitution, and Newton's experiments showed that e depended
only on the materials of which the balls were made, and not on the masses
or relative velocities^ ATseries of experiments were made by Hodgkinson,
tHeTesults ofwhich were in general agreement with Newton's. Hodgkinson
found, however {Report of British Associatio7i, 1834), that when the initial
relative^yelocity was very large e was smaller than it was with moderate
velocity.
Tincent* has shown that the coefficient of restitution is given by the
equation 6 = 6,,- bu, where u is the velocity of approach and e^ and b are
constants.
Equation (1) and the equation
mM + Mv = mU + MV (2)
• Vincent, Proceedings Cambridge Philosophical Society, vol. x p, 332.
\
I
no PROPERTIES OF MATTER.
which expresses that the momentum of the system of two bodies is not
altered by the impact, vi and M being the masses of the bodies, are sufficient
to determine U, V ; solving equations (1) and (2) we find
m + M m + M^ '
m + M m + M^ '
Hence we have
^ ■ 3,niV'+my'=^hmu' + mv'-m-e'),^^(v-uy (3)
Thus the kinetic energy after impact is less than the kinetic energy
before impact by
Thus, if e is unity there is no loss of kinetic energy. In all other cases
there is a finite loss of kinetic energy, some of it being transformed during
the collision into heat ; a small part only c-f it may in some cases be spent
in throwing the balls into vibration about theLr figures of equilibrium.
Collision of Railway Carriagres. — To get a clearer idea of what
goes on when two elastic balls impinge against each other, let us take the
case of a collision between two railway carriages running on frictionless
rails, each carriage being provided with a bufler spring. When the
carriages come into collision, the first efiect is to compress the springs, the
pressure Avhich one spring exerts on another is transmitted to the carriages,
and the momentum of the carriage that was overtaken increases, while
that of the other diminishes ; this goes on until the two carriages are
moving with the same velocity, when the springs have their maximum
compression and the pressure between them is a maximum. The kinetic
energy of the carriages is now less than it was before impact liy
and this energy is stored in the springs. The springs having reache<i
their maximum compression begin to expand, increasing still further
the momentum of the front carriage and diminishing that of the carriage
in the rear. This goes on until the springs have legained their original
length, when the pressure between them vanishes and the carriages
separate. There is now no strain energy in the springs, and the kinetic
energy in the carriages after the collision has ceased is the same as it
was before it began.
The reader who is acquainted with the elements of the differential
calculus will find it advantageous to consider the analytical solution of
the problem, which is very simple. Let .t, y be the coordinates of the
centres of gravity of the first and second carriages respectively, ^t, ^ the
strength of the springs attached to these Girriages (by the strength of
a spring we mean the force required to produce upit ej^tensioft of th©
IMPACT. ni
spring), E, T] the compressions of these springs, and P the pressure between
them; then we have
h^ = P, ^ir} = P
X- y = constant — (^ + ?;)
The solution of these equations is
r = {v- u]b)—- sinwi
^ ^ M + m
where w =./- '^^^ ; u and v are the initial velocities of tlie
V 11 + fj! Mm '
carriages, and t is measured from the instant when the collision began.
m'^ = "' {mu + M^} - -^ (u - w)cosa,«
dt M + 7«^ ^ M + «i ^
k M^ = ^^ [mw + Mv] + ^^^(» - w)coso><
Thus the springs have their maximum compression when -J-' = _ii, i.e.^
CLL etc
when (j)t = 7r/2, or f = — ; at this instant the energy stored in the first
P2 f/
9 — ^=*i'u-Mr— ! — T ^
^ fM ^^ ^fji + ^ili + m
while the energy in the second spring is equal to
h^n
^i^=U^-uy-J^,-
Mm
fi ^ ' ' n + /i' M + m
At the instant of greatest compression the amounts of energy stored I
in the two springs are inversely as the strengths of the springs.
The springs regain their original length and the collision ceases
when P = 0 — i.e., when wt = iT, or
TT _ / M?M yit + ^
this is the time the collision lasts. We see that it increases as the masses
of the carriages increase and diminishes as the strengths of the springs
increase. It is independent of the relative velocity of the carriages
before impact.
In the case of the collision between elastic bodies the elasticity of the
material serves instead of the springs in the preceding example. Th©
112
PROPERTIES OF MATTER.
bodies when they come into collision flatten at the point of contact so
that the bodies have a tinite area in common. In the neighbourhood of
this area each body is compressed ; the compression attains a maximum,
then diminishes and vanishes when the bodies separate. The theory of
the collision between elastic bodies has been worked out from this point
of view by Hertz (see Collected Papers, English Tran.slation, p. 140), who
finds expressions for the area of the surface in contact between the
colliding bodies, the duration of the contact and the maximum pre.ssure.
The duration of contact of two equal spheres was proved by llertz to
be equal to
2-9432R:/?5SiZZr
V S{v - u)f
where R is the radius of either of the spheres, s the density of the
sphere, q and <t respectively Young's modulus and Poisson's ratio for
the substance of which the spheres are made. Hamburget has measured
the time two spheres are in contact by making the spheres close an
electric circuit whilst they are in contact and measuring the time the
current is flowing. The results of his experiments are given in the
following table. They relate to the collision of brass spheres 1"3 cm.
in radius:
Relative Velocity in cm. per sec.
7-37
12-29
19-21
29-5
Duration of collision (calculated)
„ „ (observed) .
•000185
•000196
•000167
•000173
•000153
■000157
•000140
•000148
The duration of the impact is several times the gravest time of vibra-
tion of the body. In order to start such vibrations with any vigour
the time of collision would have to be small compared with the time
of vibration. We conclude that only a small part of the energy is spent
in setting the sphejes in vjbiration.
As an example of the order of magnitude of the quantities involved
in the collision of spheres we quote the results given by Hertz for two
steel spheres 2 5 cm. in radius meeting with a relative velocity of 1 cm.
per second. The radius of the surface of contact is 'OlS cm. The time
of contact is '00038 seconds. The maximum total pressure is 2'-t7
kilogrammes and the maximum pressure per unit area is 7300 kilogrammes
per square centimetre.
In this theory and in the example of the carriages with springs we
have supposed that the work dene on the springs is all stored up as
available potential energy and is ultimately reconverted into kinetic
energy, so that the total kinetic energy at the end of the impact is the
SJime as at the beginning. Tliis is the case of the impact of what are
called perfectly elastic bodies, for which the coefficient of restitution is
equal to unity. In other cases we see by equation (3) that, instead of the
whole work done on the springs being reconverted into kinetic energy,
only the constant fraction e" of it is so reconverted, the rest being ulti-
mately converted into heat. Now our study of the elastic properties of
bodies has shown many examples in which it is impossible to convert the
energy due to strain into kinetic energy and the kinetic energy back
again into energy due to strain without dissipation. We may mention
the phenomena of elastic fatigue or viscosity of metals (see page 57),
IMPACT. lis
as exemplified by the torsional vibrations of a metal wire, where the
successive transformations of the energy were accompanied by a con-
tinued loss of available energy. Again, the elastic after-effect would
prevent a total conversion of strain energy into mechanical energy.
For example, if we load a wire up to a certain point, and measure
the extension corresponding to any load, then gradually unload the
wire, if the straining has gone beyond the elastic limit the extensions
during unloading will not be the same as during loading; and in this case
there will in any complete cycle be a loss of mechanical energy proportional
to the area included between the curves for loading and unloading. The per-
centage loss in this case would depend upon the intensity of the maximum
stress; if this did not strain the body beyond its elastic limit there would
be no loss from this cause, while if the maximum strain exceeded this limit
the loss might be considerable. This may be the reason why the value
of e diminishes as the relative velocity at the moment of collision increases,
for Hertz has shown that the maximum pressure increases with the
relative velocity being proportional to the 2/r)ths power of the velocity,
while it is in(lependent of the size of the balls. Thus the greater the
relative velocity the more will the maximum pressure exceed the elastic
limit and the larger the amount of heat produced. In addition to
the loss of energy by the viscosity of metals and hysteresis there is
in many cases of collision permanent deformation of the surface in
the neighbourhood of the surface of contact. This is very evident
in the case of lead and brass. The harder the body the greater the value
of e. We can see the reason for this if we remember that the hardness
of a body is measured by the maximum stress it can suffer without
being strained beyond the elastic limit, while any strain beyond the
elastic limit wotdd increase the amount of heat produced and so diminish
the value of e.
When we consider the various ways in which imperfections in the
elastic property can prevent the complete transformation of the energy due
to strain into liinetic energy and vice versa, it is somewhat surprising that
the laws of the collision of imperfectly elastic bodies are as simple as
Newton's and Hodgkinson's experiments show them to be, for these laws
expi-ess the fact that in the collision a constant fraction, e^, of the initial
kinetic energy is converted into heat, and that this fraction is independent
of the size of the spheres and only varies very slowly with the relative
velocity at impact. For example, Hodgkinson's experiments show that
when the relative velocity at impact was increased threefold the value of «
in the case of the collision between cast-iron spheres only diminished from
•69 to "59. A series of experiments on the impact of bodies meeting with
very small relative velocities would be very interesting, for with small
velocities the stresses would diminish, and if these did not exceed those
corresponding to elastic limits some of the causes of the dissipation of
energy would be eliminated, and it is possible that the value of e might
be considerably increased.
We find, too, from experiment that bodies require time to recover even
from small strain, so that, if the rise and fall of the stress is very rapid,
there may be dissipation of energy in cases where the elastic limit for
slowl)' varying forces is not overstepped.
Hodgkinson gives the following formula for the value of e^B? when two
different bodies A and B collide, in terms of the values of e^A ^or the
H
114
PROPERTIES OF MATTER.
collision between two bodies each of material A and e^B, the value for the
collision between two bodies each of material B.
*AB —
and he finds this formula agrees well with his experiments.
The following considerations would lead to a formula giving c^b ^^
terms of e^A ^^^^ ^bb- Hertz has shown that the displacements of the
bodies A and B in the direction of the common normal to the two surfaces
over which the bodies touch are proportional to
Lz:^' and 1^5.'
^AA
^^BB
9,
9,
1
-f-1
9i
92
9x 9i
where <Tp a.^ are the values of Poisson's ratio for the bodies A and B and
5",, q^ the values of Young's modulus. Now the stresses are equal, so that,
assuming that the quantities of work done on the two bodies are in the
ratio of the displacements, then, if E is the whole work done,
^-^E
1 - a.:
E
+
1-
"i and
izV + i^^
9i 92 9i 92
will be the amounts done on the two bodies. Now the first body converts
1 - e^A fii^d the second 1 - e-^^ of this work into heat ; hence the energy
converted into heat will be
9x 92_
and this must equal
e-
AA
9i 92
(l-e\B)E
E
^ BB ■
hence
* AB =
1-:
1-,
The following table of the values of e is taken from Hodgkinson's
Report to the British Association, 1834 :
Dast-iron balls .
•66
Clay .
Oast-iron — lead .
•13
Clav — soft brass
Cast-iron — boulder stone .
•71
Glass ,
Boulder stone— brass .
■62
Cork .
Boulder stone — lead .
•17
Ivory .
Boulder stone — elm .
. •oe
Lead — glass
Elm balls ....
•60
,Soft brass — glass
Soft brass (16 pt. Cu. and 1 pt.
tin
) -36
Bell metal — glass
Bell metal (16 pt. Cu. and 4 pt.
tin
) -59
Cast-iron — glass
Lead . . . . •
. ^20
Lead -ivory
Lead — elm ....
. ^41
Soft brass— ivory
Elm — »oft brass .
. -52
Bell metal — ivorj
17
16
94
65
81
25
78
87
91
44
78
77
IMPACT. 113
The case where a permanent deformation is produced has recently been
investigated by Vincent {Proceedivgs Cambridge Philosophical Society,
vol. X. p. 332). The case taken is that of the indentation produced in lead
or pai-affin by the impact of a steel sphere. He finds that the volume of
the dent is proportional to the energy of the sphere just before impact ;
that during the impact {i.e., while the lead is flowing) the pressure between
the sphere and the lead is constant and varies from 6 x 10** to 13 x 10'* dynes
per square centimetre f<ir different specimens of lead ; for parafiin the
corre=!ponding pressure is about 10" dynes per square centimetre.
CHAPTEH XL
COMPRESSIBILITY OF LIQUIDS.
Contents.— Changes in Volume of a Tube unrlcr Internal and External Tresvure —
Measurements of Corapressibilitv of Liquids by methods of Jamin, Regnault,
Buchanan and Tait, Aniagnt- Comi)resfibility of Water— Effects of Temperature
and Pressure— Compressibility of Mercury and other Liquids— Tensile Strength
of Liquids.
The fact that water is compressible under pressure was establishctl in 17G2
by Canton, and since then measurements of the changes of volume of
liquids under pressure have been made by many physicists.
The problem is one beset with experimental ditficulties, some of which
may be illustrated by considering the case of a liquid inclosed in a vessel
such as a thermometer; when pressure is applied to the liquid, the
depression of the liquid in the stem will be due partly to the contraction
of the liquid under pressure and partly to the expansion of the bulb of the
thermometer. In order, then, to be able to determine from the depression
of the liquid the compressibility of water we must be able to estimate the
alteration in volume of the tube under pressure. We shall therefore
consider in some detail the alteration in volume of a vessel subject to
internal and external pressui-e. We shall take the case of a long cylindrical
tube with flat ends exposed to an external pressure p^ and an internal
pressure jo^. The strain in such a cylinder has been shown by Lame
to be (1) a radial displacement p given by the equation
p = A?- + -
r
where r is the distance of the point under consideration from the axis of
the cylinder and A and B constants, and (2) an extension parallel to the
axis of the cylinder.
The radial displacement p involves an elongation along the radius equal
to dpjdr and an elongation at right angles to p in the plane at right angles
to the axis of the cj'linder equal to pjr. Let the elongations along the
radius, at right angles to it and to the axis of the cylinder, and along the
axis be denoted by e, f, g respectively, and let P, Q, E, be the normal
stresses in these directions ; then by equation (1 ), p. 72, we can easily prove
'^. '^.'' -n ft . 4n\ . /, 2n\
where k is the bulk modulus and n the coefficient of rigidity.
0)
r
COMPRESSIBILITY OF LIQUIDS. 117
Since e= f and f=^
dr r
we have e = A - - , /= A + —
Thus the radial stress is equal to
o
2/.A + =^lA-^Vf^-??V
n
•6\ 1- ) \ 3/
If a and h are respectively the internal and external radii of the tube,
then when r = a the radial stress is equal to —p^ and when r = h the radial
stress is equal to — ^j, hence we have
-,.= 2M4f(A-??).(.-|'), (2)
The whole force parallel to the axis tending to stretch the cylinder i.->
Trd-p^ - nb-p^
hence the stress in this direction is equal to
na-po - 7ri7?i
7r{b'' - a-)
The stress parallel to the axis is, however, equal to
(.4)..(.--).A
hence we have
From (2), (;3) and (4) we get
and ^ = 2i^(¥-^f''"-P^^ | (^"^
Since the radial displacement is Ar+— , the internal volume of the
tube when sti-ained is n(a + Aa + —]'l{l+g) A/9(
•■'*- where Hs the length of the tube; hence, retaining only the first powers
v-''^, of the small quantities A, B and g, we b-ave, if cv^ is the change in the
internal volume,
-Lf
- ;'• /. ^A.\
118 PROPERTIES OF MATTER.
and if 3y, is the change in the external volume,
I b' -a- k^ 0- - a' n J
Methods of Measuring" Compressibility of Liquids. — There are
two cases ot" s^jecial iinportaiice in the determination of the compressibility
of fluids : the first is when the internal and external pressures are equal ;
in this case Pq=j>v '^^^ ^® have
TTClH
T
^^1= --jrPo
Thus the diminution of the volume is independent of the thickness of the
walls of the tube. Some experimenters have been led into error by supposing
that, if the walls of the tube were very thin, there would be no appreciable
diminution in the volume of the tube. If the vessel had been filled with
liquid which was subject to the pressure p^, the diminution in the volume
of the liquid would be Tra"lpJK, where K is the bulk modulus of the liquid.
The diminution of volume of the liquid minus that of the vessel is
therefore
'^"^^E"^)
thus by experiments with equal pres.sui-es inside and out, which was
Regnault's method, we determine
11
K k
so that to deduce K we must know k.
Another method, used by Jamin, waste use internal pressure only, when
the apparent change in the volume of the liquid is the sum of the changes
of volumes of the liquid and of the inside of the vessel. Jamin thought
that he determined the change of volume of the vessel by placing it in an
outer vessel full of water and measuring the rise of the water in a gradu-
ated capillary tube attached to this outer vessel ; by subtracting this change
in volume from the apparent change he thought he got the change in
volume of the liquid without requiring the values of the elastic constants
of the material of which the vessel is made. A little consideration will
show, however, that this is not the case. Let cv be the change in the
volume of the liquid, Sr, the change in the internal volume, h\ that in the
external volume; it is oi'^ that is measured by the rise of liquid in the
capillary tube attached to the vessel containing the tube in which the
liquid is compressed.
Observations on the liquid inside the tube give
Sv + Svj
if we subtract Jamin's correction we get
Sv + h\ - Svj
substituting the values of h\ and Sr^ when 7?j = o we find
h + Si', -di\ = ov- — -^-5- and dv = — ^
COMPRESSIBILITY OF LIQUIDS.
119
f 1 V
■-.--] the same
Hence, after applying Jamin's correction, we get naHpJ t> ~ r
quantity as was determined by Regnault's method, so that to get K by
Jamin's method we require to know k.
The apparatus used by Rcgnault in his experiments on the comf>r66si-
bility of Hquids (Memoires de VInstitut de France,
vol. xxi. p, 429) was similar to that represented in
Fig. 82. The piezometer was filled with the liquid
whose compressibility was to be measured, the
greatest care being taken to get rid of air-bubbles,
The liquid reached up into the graduated stem of the
piezometer, the volume between successive marks on
the stem being accurately known. The piezometer
was placed in an outer vessel which was filled with
water and the whole system placed in a large tank
filled with water, the object being to keep the
temperature of the system constant. The tubes
shown in the system were connected with a vessel
full of compressed air, the pressure of which was
measured by a carefully tested manometer ; the
tubes were so arranged that by turning on the
proper taps pressure could be applied (1) to the
outside of the piezometer and not to the inside ; (2)
simultaneously to the outside and the inside ; (3) to
the inside and not to the outside. The piezometer
used by Regnault was in the form of a cylindrical
tube with hemispherical ends. For simplicity let
us take the case (represented in the figure) of a piezometer in the form of
a cylinder with flat ends, to which the foregoing investigation applies.
If Wp Wj, W3 are the apparent diminution in the volume of the liquid in
the three cases respectively, the pressure being the same, we have by the
preceding theory
ira?hH /I , 1\
Fig. 82.
(t)
b)
Hence Wj + Wj = wg
a relation by which we can check to some extent the validity of the
theoretical investigation. Such a check is very desirable, as in this investi-
gation we have assumed that the material of which the piezometer is made
is isotropic and that the walls of the piezometer are of unifoi-m thickness,
conditions which are very difficult to fulfil, while it is important to
ensure that a failure in any one of them has not been sufficient to
appreciably impair the accuracy of the theoretical investigations. Regnault
in his investigations adopted Lamp's assumption that Poisson's ratio ia
3
equal to 1/4 ; on this assumption n = -A;, so that the measurement of Wj
0
120
PROPERTIES OF MATTER.
gives the value of Jc, and then the measurement of w^ the value of K, the
bulk modulus for the liquid. This was the method adopted by Regnault.
It is, however, open to objection. In the first place, the determinations
which have been made of the value of Poisson's ratio for glass range from
•33 to "22, instead of the assumed value "25, while, secondly, the equation by
which k is determined from measurements of Wj is obtained
on the assumption of perfect uniformity in the material
which it is difficult to verify. It is thus desirable to
determine k for the material of which the piezometer is
made by a separate investigation, and then to determine the
compressibility of the liquids by using the simplest relation
obtained between the apparent change in volume of the liquid
and the pressure ; this is when the inside and outside of the
piezometer are exposed to equal pressures. The most direct,
and probably the most accurate, way of finding k for a solid is
to measure the longitudinal contraction under pressure. An
arrangement which enables this to be done with great
accuracy is described by Amagat in the Journal de Physique,
Series 2, vol. viii. p. 359. The method was first used by
Buchanan and Tait. Another method of determining k for
a solid is to make a tube of the solid closed by a graduated
capillary tube as in Fig. 83. The tube and part of the
capillary being tilled with water, a tension P is applied to the
tube, the tube stretches and the internal volume increases, the
increase in volume being measured by the descent of the liquid
in the capillary tube ; if v is the original internal volume, Su
the increase in this volume, then we see by the inve.stigation,
p. 12, that
£y^P
V '6k
If we have found k, then K can be found by means of the
piezometer.
If we can regard the compressibility of any liquid, say
mercury, as known, the most accurate way of finding tha
compressibility of any other liquid would be to fill the
piezometer first with mercury, and determine the apparent
change of volume Avhen the inside and outside of the
piezometer are exposed to the same pressure ; then fill the
piezometer with the liquid and again find the apparent change
in volume. We shall thus get two equations from which we
can find the value of K for the liquid and k for the piezometer.
Results of Experiments. — The results of experiments made by
diflerent observers on the compressibility of water are given below.
Regnault.* — Temperature not specified ; pressures from 1 to 10 atmo-
spheres—
compressibility per atmosphere = 0.0000 18.
Fio. 83.
* Mimoircs de Vlnstitut de France, vol. xxi. p. 429.
COMPRESSIBILITY OF LIQUIDS.
121
GKASSI.*
PAGLIANIand VICENTINI.t
RONTGEN and SCHNEIDER. J
Temp.
Compressibility
pel' atmosxjheie.
Temp.
Compressibility
per atmosphei..
Temp.
Compressibility
per atmosphere.
00
1-5
4-0
max. density
pt.
10-8
13-4
18-0
25.0
34-5
430
530
503x10-''
515
499
480
477
462
456
453
412
441
0.0
2-4
15-9
49-3
61-1
C6-2
77-4
99.2
503x10-''
496
450
403
389
389
398
409
0 0
9-0
18-0
512x10-7
4S,1
462
Tait§ has found that the efiect of temperature and pressure, for
temperatures between 6° 0. and 15° 0. to pressures from 150 to 500
atmospheres, may be represented by the empirical formula
IiLlJ' = 0-0000489 - 0-00000025^ - 0.0000000067o
where v is the volume at f C. under the pressure of p atmospheres and v
the volume at f° under one atmosphere. Thus the compressibility diminishes
as the pressure increases.
The numbers given above, from Grassi's experiments, indicate that
water has a maximum compressibility at a temperature between 0° and 4:° C:
this result has not, however, been confirmed by subsequent observers. The
I'esults of Pagliani and Vicentini indicate a minimum compressibility at
a temperature between 60° and 70° 0.
The results of various observers on the compressibilit}' of mercury are
given in the following table :
Com pressibility
per atmosphere.
Observer.
Colladon and Sturm H ,
Aime^ . . . .
Regnault**
Amaury and Descamp> ft
JLait^.^ . . . .
Amagat§§
De Metzllll
Mean . . . .
35-2x10-'
39-0x10-'
35-2x10-^
38-6x10-^
36-0x10-''
39-0x10-'
37-4x10-'
37-9x10-'
The compressibility of mercury, like that of most fluids, increases as the
* Gras.si, Annalcs de C'himic ct de Physique [3], 31, p. 437, 1851.
f Pagliani and Vicentini, Nuovo Cimento [3], 16, p. 27, 1884.
X Rontgen and Schneider, Wicd. Ann., 33, p. 644, 1888.
§ Tait, Properties of Matter, 1st ed. (1885), p. 190.
II Colladon and Sturm, Ann. de Chimie et de Physique, 36, p. 137, 1827.
«I Airae, Annah.f de Chimie et de Physique [3], 8, p. 268. 1843.
** Eegnault, Memoires de I'lnstitut de France, 21, p. 429, 1847.
tt Araaury and Descarops, Compt. Rend., 68, p. 1564, 1869.
+t
Tait, Challenger Report, vol. ii. part iv.
§§ Amagat, Journal de Physique [2], 8, p. 203, 1889.
nil De Metz, Wicd. Ann., 47, p. 731, 1892.
122
PROPERTIES OF MATTER.
temperature increases. According to De Metz, the compressibility at t" 0.
is given by
37-4 X 10-' + 87-7 xlO-"«
The compressibilities of a number of liquids of frequent occurrence are
given below.
Fluid.
Conipressiliility per
atinospliere.
Temp.
Observer.
Sea-water ,
Ether .
11 • •
Alcohol
11 • I
11 • I
Methyl alcohol
Turpentine .
11 •
Chloroform .
Glycerine .
Olive oil
Carbon bisulphid
11 II
Petroleum .
e
436x10-7
1156x10-7
1110x10-7
828x10-7
959x10-7
828x10-7
913x10-7
682x10-7
779x10-7
625x10-7
252x10-7
486x10-7
539x10-7
038x10-7
650x10-7
745x10-7
17-5°
0°
0°
0°
17-5'
7-3°
13-5"
0°
18-6
8-5-
0°
0°
0°
17°
0°
19-2'
Grassi
Quincke
Grassi
Quincke
Grassi
fj ■
Quincke
11
Grassi
Quincke
»
II
II
II
»
waters
V
Quincke's paper is in Wiedemanns Anndlen, 19, p. 401, 1883. Eeferences to
the papers by the other observers have already been given. An exten-
sive series of investigations on
the compressibility of solutions
has been made by Rontgen
and Schneider {Wied. Ann., 29,
p. 16 5, and 81, p. 1000), who have
shown that the compressibility
of aqueous solutions is less
than that of water. For the
details of their results we must
refer the leader to their paper.
Tensile Streng-th of
Liquids. — Liquids from which
the air has been carefully ex-
pelled can sustain a considerable
pull without rupture. The best
known illustiation of this is
the sticking of the meicury at
the top of a barometer-tube.
If a barometer-tube filled with
mercury be carefully tilted up
to a vertical position, the mer-
cury sometimes adheres to the
top of the tube, and the tube remains filled with mercury, although the
length of the column is gieater than that which the normal barometric
pressure would support, and the extra length of mercury is in a state of
tension. Another method of showing that liquids can sustain tension
water vapour
COMPRESSIBILITY OF LIQUIDS.
123
without rupture is to use a tube like that in Fig. 84, filled with water and
the vapour of water, and from which the air has been eai*efully expelled
by boiling the water and driving the air out by the steam.* If the water
occupies the position indicated in the figure, the tube mounted on a board
may be moved rapidly forward in the direction of the arrow, and then
brought suddenly to rest by striking the board against a table without the
water column breaking, although the column must have experienced a
considerable impulsive tension. If the column does break, a small bubble
of air can generally be observed at the place of rupture, and until this
bubble has been removed the column will break with great ease. On the
removal of the bubble by tapping, the column can again sustain a con-
siderable shock without rupture.
Professor Osborne Reynolds used the following method for measuring
the tension liquids would stand without breaking. ABCD, Fig. 85, is a
glass U-tube, closed at both ends, containing air-free liquid ABO and
vapour of the liquid CD. The tube is fixed to a board and whirled by a
lathe about an axis O a little beyond the end A and perpendicular to the
plane of the board. If CE is an arc of an circle with centre O, then when
the board is rotating the liquid EA is in a state of tension,
the tension increasing from E to A, and being easily
calculable if we know the velocity of rotation. By this
method Professor Osborne Reynolds found that water could
sustain a tension of 72 "5 pounds to the square inch without
rupture, and Professor Worthington, using the same method,
found that alcohol could sustain 116 and strong sulphuric
acid 173 pounds per square inch. This method measures the
stress liquids can sustain without rupture. Berthelot has
used a method by which the strain is measured. The liquid
freed from air by long boiling nearly filled a straight thick-
walled glass tube, the rest of the space being occupied by the
vapour of the liquid. The liquid was slightly heated until it
occupied the whole tube; on cooling, the liquid continued for
some time to fill the tube, finally breaking with a loud
metallic click, and the bubble of vapour reappeared : the length of this
bubble measured the extension of the liquid. M. Berthelot in this way
got extensions of volume of 1/120 for water, 1/93 for alcohol, and 1/51) for
ether. Professor Worthington has improved this method by inserting in
the liquid an ellipsoidal bulb filled with mercury and provided with a
narrow graduated capillaxy stem ; when the liquid is in a state of tension
the volume of the bulb expands and the mercury sinks in the stem ; from
the amount it sinks the tension can be measured. The extension was
measured in the same way as in Berthelot's experiments. In this way
Professor Worthington showed [Phil. Trans. A. 1892, p. 355) that the
absolute coeflicient of volume elasticity for alcohol is the same for
extension as for compression, and is constant between pressures of + 12
and — 17 atmospheres.
* Dixon and Joly (Pldl. Trans. B. 1895, p. 568) have shown that air or other gases
held in solution do not afltect these experiments. The bojling is probablj^ efficacious
ooly in removing bubbles or free gases,
0
Fia. 85.
CHAPTER XII.
THE RELATION BETWEEN THE PRESSURE AND VOLUME
OF A GAS.
Contents— Boyle's Law— Deviations from Bovle's Law— Fegnault's Experiments—
Amagat's Experiments — Experiments at Low rre.s»urcs — Van der Waals' Equation.
In this chapter we shall confine ourselves to the discussion of the relation
between the pressure and the volume of a gas when the temperature is
constant and no change of state takes place ; the liquefaction of gases
will be dealt with in the volume on Heat.
The relation between the pressure and the volume of a given mass of
gas was first stated by Boyle in a paper communicated to the Royal Society
in 1061. The experiment which led to this law is thus described by him.
" We took then a long glass tube, which by a dexterous hand and the help
of a lamp was in such a manner crooked at the bottom, that the part
turned up was almost parallel to the rest of the tube, and the orifice of
this shorter leg of the siphon (if I may so call the whole instrument) being
hermetically sealed, the length of it was divided into inches (each of which
was subdivided into eight parts) by a straight list of paper, which, con-
taining those divisions, was carefully pasted all along it. Then putting in
as much quicksilver as served to fill the arch or bended part of the siphon,
that the mercury standing in a level might reach in the one leg to the
bottom of the divided paper and just to the same height or horizontal line
in the other, we took care, by frequently inclining the tube, so that the
air might freely pass from one leg into the other by the sides of the
mercury (we took, I say, care), that the air at last included in the shorter
cylinder should be of the same laxity with the rest of the air about it.
This done, we began to pour quicksilver into the longer leg of the siphon,
which by its weight pressing up that in the shoi-ter leg did by degi-ees
strengthen the included air, and continuing this pouring in of quicksilver
till the air in the shorter leg was by condensation reduced to take up but
half the space it possessed (I say, possessed not filled) before, we cast our
eyes upon the longer leg of the glass, on which was likewise pasted a list
of paper carefully divided into inches and parts, and we observed not
without delight and satisfaction that the quicksilver in that longer part
of the tube was 29 inches higher than the other . . . the same air
being brought to a degree of density about twice as great as that it had
befoi-e, obtains a spring twice as strong as formeily." Boyle made a series
of measurements with greater compressions until he had reduced the
volume to one quarter of its original value, and obtained a close agreement
between the pressure observed and " what that pressure should be according
to the hypothesis that supposes the pressures and expansions*to be in
reciprociil proportions." Although Mariotte did not state the law until
fourteen years after Boyle had published his discovery, " the hypothesis
* Or volumes, in modern Euglisli.
THE PRESSURE AND VOI,UME OF A GAS. 125
that supposes the pressures and expansions to be in reciprocal proportions "
is often on the Continent called Mariotte's Law.
If V is the volume of a given mass of gas and p the pressure to which
it is subjected, then Boyle's Law states that when the temperature is
constant
pv = constant.
Anotlier way of stating this law is that, if p is the density of a gas under
pressure p,
p = 'Rp,
where R is a constant when the temperature is constant. Later researches
made Vjy Charles and Gay-Lussac have shown how R varies with the
temperature and with the nature of the gas. These will be described in
the volume on Heat ; it will suffice to say here that the pressure of a perfect
gas is given by the equation
;> = KNT,
where T is the absolute temperature, N the number of molecules of the gas
in unit volume, and K a constant which is the same for all gases.
From the equation pv = c we see that if Aj), Av are corresponding incre-
ments in the pressure and volume of a gas whose temperature is constant,
then
or - — ^ =Pi
Av
but the left-hand side is by definition the bulk modulus of elasticity,
hence the bulk modulus of elasticity of a gas at a constant temperature is
equal to the pressure.
The work required to diminish the volume of a gas by Av is pAv ; the
work which has to be done to diminish the volume from v^ to v^ is there-
fore
j pdvy
or, since by Boyle's Law p = c/v, when the temperature is constant, we
see that in this case the work is
c -dv = c log,-i =;; Vjlog,'^ ,
J V ^j ^«
where />, is the pressure when the volume is w,.
Deviations from Boyle's Law. — The first to establish in a satis-
factory manner the existence in some gases, at any rate, of a departure from
Boyle's Law was Despretz, who, in 1827, enclosed a number of different
gases in barometer-tubes of the same length standing in the same cistern.
The quantity of the different gases was adjusted so that initially the mercury
stood at the same height in the diflerent tubes ; pressure was then applied
to the mercury in the cistern, so that mercury was forced up the tubes.
It was then found that the volumes occupied by the gases were no longer
126
PROPERTIES OP MATTER.
equal, the volumes of carbonic acid and ammonia were less than that of
air, -while that of hydrogen was greater. This showed that some of the
gases did not obey Boyle's Law; it left open the question, however, as to
whether any gases did obey it. The next great advance was made by
llegnaultf who in 1847 settled the question as to the behaviour of certain
gases for pressures between 1 and about 30 atmospheres, llegnault's
method was to start with a certain quantity of gas occupying a volume v
in a tube sealed at the upper end, and with the lower end opening into a
closed vessel full of mercury, and then by pumping mercury up a long
mercury column rising from the closed vessel to increase the pressure until
the volume was halved . By measuring the difference of height of
mercuiy in the column and in the tube the pressure required to do this
could be determined. Air under this pressure was now pumped into the
closed tube until the volume occupied by the gas was again v ; mercury
was again pumped up the column until the volume had again been halved
and a new reading of the pressure taken ; air was pumped in again until
the volume was again 7;, and then the pressure increased again until the
volume was halved. In this way the values oi pv at a series of different
pressures could be compared. The results are shown in the following
table
, -p^ is given in millimetres of mercury, /)„?'„ is the value of pv at the
pressure given in the table, p^^ the value at double this pi-essure. The
experiments were made at temperatures between T C. and 10° C.
AIR.
NITROGEN.
CARBONIC ACID.
HYDROGEN.
Vo
'PoVollh'Vl
Po
PoVoIPiVi
Po
PoVolPiVy
Po
PoVolp^y^
73S72
1-001414
753-96
1-001012
764-03
1-007597
2068-20
1-002709
1159-43
1-001074
1414-77
1-012313
4219-05
1-003336
2159-22
1-001097
2164-81
1-018973
2211-18
0-998.^.84
6770-15
1-004286
3030-22
1-001950
3186-13
1-028494
3989-47
0-996961
9336-41
1-006366
4953-92
1-002952
4879-77
1-045625
5845-18
0-9961-21
11472-00
1-005619
5957-96
1-003271
6820-22
1-066137
7074-96
0-994697
7294-47
1-003770
8393-68
1-084278
9147-61
0-993258
8628-54
1-004768
96-20-06
1-099830
10361-88
0-992327
9767-42
1-005147
10981-42
1-006456
It will be seen from these figures that between pi'essures of from about
1 to 30 atmospheres the product pv constantlydiminishes for air, nitrogen,
andjcarbonic acid, as the pressure increasesTTFie diminution being most
marked forcarbonicacid ; on the other hand in h3'drogen pv increases with
The pressure. JNatterer^who in 1850 published the results of experiments
on the relation between the pressure and volume of a gas at very high
pressure, showed that after passing certain pressures ^w for air and nitrogen
begins to increase, so that pv has a minimum value at a certain pressure;
after passing this pres.sure air and nitrogen resemlile hydrogen, and pv
continually increases as the pressure increases. This result was confirmed
by the researches of Amagat and Cailletet. Eaoii of these physicists worked
at tlie bottom of a mine, and produced their pressures by long columns of
ineicury in a tube going up the shaft of the mine. Amagat's tube waa
300 metres long, Cailletet's 250. Amagat found that the minimum value
ol pv between 18° and 22° C. occurred at the following pressures:
* Mdmoires de V Institut de France, vol. xxi. p. 329,
THE PRESSURE AND VOLUME OF A GAS.
127
Nitrogen .
50 metres of mercury
Oxygen .
. 100
Air .
65 „ „
Carbon monoxide 50 metres of mercury.
Marsh gas ,120 „ „
Ethylene . 65 „
The results of his experi-
ments arc cxhil)ited in the fol-
lowing figures ; the ordinates are
the values oi pv, and the abscissse
the pressure, the unit of pressure
being the atmosphere, which is
the pressure due to a column of
mercury 7 GO mm. high at 0° C,
and at the latitude of Paris.
The numbers on the curves indi-
cate the temperature at which
the experiments were made. It
will be noticed that for nitrogen
the pressure at which pv is a
minimum diminishes as the tem-
perature increases, so much so
that at a temperature of about
100° 0. the minimum value of
pv is hardly noticeable in the
curve. This is shown clearly by
the following results given by
Amagat :
Fia. 86.— Ethylene
IT-r C.
30-1° C.
50-4° C.
75-5° C.
lOO-r C.
p
pv
po
pv
pv
pv
30 metres
2745
2875
3080
3330
3575
60 „ ...
2740
2875
3100
3360
3610
100 „ ...
2790
2930
3170
3445
3695
200 „ ...
3075
3220
3465
3750
4020
320 „ ...
3525
3675
3915
4210
4475
Amagat extended his experiments to very much higher pressures, and
obtained the results shown in the following table ; the temperature was
15" C, andpv was equal to 1 under the pressure of 1 atmosphere:
p (in atmospheres).
Air.
J>0
Nitrogen.
pv
Oxygen.
pv
Hydrogen.
pv
750
1-650
1-6965
_
„
1000
1-874
2-032
1-735
1-688
1500
2-563
2-644
2-238
2-016
2000
3-132
3-2-20
2-746
2-322
2500
3-672
3-787
3-235
2-617
3000
4-203
4-338
3-705
2-892
\
A question of considerable importance in these experiments, and one
(vhich we have hardly sufficient information to answer satisfactorily, arises
from the condensation of gas on the walls of the manometer, and possibly
a penetration of the gas into the f-ubstance of these walls. It is well known
128
PROPERTIES OF MATTER.
Fig. 87.— Nitrogen.
that when we attempt to exhaust a glass vessel a considerable amount of
gas comes off the glass, and if the vessel contains pieces of metal the
difficulty of getting a vacuum is still further increased, as gas for some time
continues to come from the metal. Much of this is, no doubt, condensed on
the surface, but when we
remember that water can
be forced through gold it
seems not improbable that
at high pressure the gas
may be forced some dis-
tance into the metal as
well as condensed on its
surface.
Boyle's Law at Low
Pressures. — The diffi-
culty arising from gas com-
ing off the walls of the
manometer becomes spe-
cially acute when the pres-
sure is low, as here the
deviations from Boyle's Law are so small that any trifling error may
completely vitiate the experiments. This is probably one of the reasons
why our knowledge of the relation between the pressure and volume of
g:vses at low pressures is so unsatisfactory, and the results of different
experiments so contradictory. According to Mendeleeff, and his result has
been confirmed by 'Fuchs, pv for air at pressures below an atmosphere
diminishes as the pressure
diminishes, the value of pv
changing by about 3-5 per
cent, between the pressure
of 7G0 and 14 mm. of
mercury. If thi? is the
case, then pv for air has a
maximum as well as a mini-
mum value. On the other
hand, Amagat, who made
a series of very careful
experiments at low pres-
sures, was not able to detect
any departure from Boyle's
^ Fig. 88.-Hydrogen, Law. According to Bohr,
and his result has been
confirmed by Baly and Bamsay, the law connecting p and v for oxygen
changes at a pressure of about '75 mm. of mercury. It has been
suggested that this is due to the formation of ozone. The recent
investigations by Lord Rayleigh on the relation between the pressure and
volume of gases at low pressures do not show any depai-ture from
Boyle's Law even in the case of oxygen.
The results of Amagat's experiments are in fair accordance with
the relation between p and v, arrived at by Van der Waals from
the Kinetic Theory of Gases. This relation is expressed by the
equation
THE PRESSURE AND VOLUME OF A GAS.
129
(p + ^^{v-b) = UT
v here a, h, II are constants and T is the absolute temperature. Thus p in
Boyle's equation is replaced by p + a/v- and vhy v — b. The term a/v- or
a|0-,wherejois the density, arises from the attractions between the molecules
of the gas ; this attraction assists the outside pressure to diminish the
volume of the gas. If we imagine the gas divided by a plane into two
portions A and B, then ap^ is the attraction of A on B per unit area of the
plane of separation ; it is the quantity we call the intrinsic pressure in the
pv
Fio. 89.
theory of Capillarity (see chap. xv). The v of Boyle's Law is replaced by
v — b. Since the molecules are supposed to be of a finite although very
small size, only a part of the volume "occupied" by the gas is taken up
by the molecules, and the actual volume to be diminished is the difference
between the space "occupied " by the gas and that filled by its molecules;
b is proportional to the volume of a molecule of the gas.
Van der Waals' equation may be written :
ht){'-l
RT
so that if
we have
pv = p and - =p
■x.
V
(2/ + ax){l-b.v) = nT
Thus, if the temperature is constant, the curve which represents the rela-
tion between pv and p is the hyperbola
{y + ax) (1 - bx) = constant.
130 PROPERTIES OF MATTER.
The asymptotes of this hyperbola are y + ax = o, 1 — &a; = 0. There is a
minimum value of pv at the point P (Eig. 89) where the tangent is horizontal.
The value of x at this point is easily shown to be given by the equation
a{\-hxf = hllT.
If &RT/a is less than unity there is a ])ositive value of x given by this
equation. This corresponds to the minimum value for pv in the cases of air,
nitrogen, and carbonic acid. We see, too, from the equation that as T
increases x diminishes, that is, the pressure at which the minimum value
oi pv occui-s is lower at high temperatures than at low. This agrees with
the results of Amagat's experiments on nitrogen. When T gets so large
that 6RT/a is unity x — Q; at all higher temperatures it is negative — i.e.,
P is to the left of the vertical axis, there is thus no minimum value of pv,
and the gas behaves like Lydro^en in that^^7 continually increases' ys the
pressure increaisea.
CHAPTER XIII.
REVERSIBLE THERMAL EFFECTS ACCOMPANYING
ALTERATIONS IN STRAINS.
Contents. — Application of Thermodynamics — Ratio of Adiabatic to Isothermal
Elasticity.
^C'. -.>- - c
If the coefficients of elasticity of a substance depend upon the tempera'
ture an alteration in the state of strain of a body will be accompanied
by a change in its temperature. If the body is stifler at a high tern- .,.
perature than at a low one, then, if the strain is increased, there will , JCi^L
be an increase in the temperature of the strained body, while if the body ^^ ., / > /
is stifter at a low temperature than at a high one, there will be a fall
in the temperature when the strain is increased. Thus, if the changes in
strain in any experiment take place so rapidly that the heat due to these
changes has not time to escape, the coefficients of elasticity determined
by these experiments will be larger than the values determined by a
method in which the strains are maintained constant for a sufficiently long
time for the temperature to become uniform ; this follows from the fact
that the thermal changes which take place when the strains are variable
are always such as to make the body stiffer to resist the change in strain.
In those experiments by which the coefficients of elasticity are determined
by acoustical methods — i.e., by methods which involve the audible vibration
of the substance {see Sound, p. 125) — the heat will not have time to dijBfuse,
and we should expect such methods to give higher values than the statical
ones we have been describing. When we calculate the ratio of the two
coefficients we find that the theoretical difference is far too small to
explain the considerable excess of the values of the constants of elasticity
found by Wertheim by acoustical methods over those found by statical
methods.
We can easily calculate by the aid of Thermodynamics the thermal
effects due to a change of strain. To fix our ideas, suppose we have two
chambers, one maintained at a temperature T,,, the other at the tempera-
ture Tj*, these temperatui-es are supposed to be absolute temperatures, and '
T(, to be less than Tj. Let us suppose that we have in the cool chamber a
stretched wire, and that we increase the elongation e by oe ; then if P is the
tension required to keep the wire stretched, the work done on the wire is
PaZae
where a is the area of the cross-section and I the length of the wire. Now
transfer the wire with its length unaltered to the hot chamber, and for
simplicity suppose the thermal capacity of the wire exceedingly small, so
that we can neglect the amount of heat required to heat up the wire ;
if the stiffness of the wire changes with temperature the tension P*
required to keep it stretched will not be the same as P. Let the wire
132 PROPERTIES OF MATTER.
contract in the hot chamber until its elongation diminishes by 5e, then the
work done by the wire is
Valde,
Now transfer the wire with its length unaltered back to the cold chamber ,
it will now be in the same state as when it started. The work done by
the wire exceeds that done on it by
hence the arrangement constitutes a heat engine, and since it is evidently
reversible it must obey the laws of such engines. These engines work
by taking heat oH from the hot chamber and giving oh out in the colder
cliamber, and from the Second Law of Thermodynamics we hava
m_hh_m-^h
T T T - T
J-, J-o -Lj J-0
Now by the Conservation of Energy
^H - ch = mechanical work done by the engine
«=(F-P)aZae;
hence SA = T}— — p— 'a Ide
-L| ~ J-o
^TM\:dce .
e constant
-01 grj,
Now Ih is the amount of heat given out by the wire when the elongation
is increased by ce, and al is the volume of the wire ; hence the mechanical
equivalent of the heat given out per unit volume, when the elongation is
measured by ^e, is equal to
\ 0 J- / e constant
If this heat is prevented from escaping from the wire it will raise the
temperature, and if cQ is the rise in temperature due to the elongation
^CjWe see that
se=TA|Ei"''"""'xj« (1)
JKp
where p is the density of the wire, K its specific heat, and J the mechanical
, equivalent of heat. We see that this expression proves the statement
made above, that the_temperature change which takes place on a change in
the strain is alwavs~such as^tomake^ tlic body .stiJjkaJto resist tiie change.
•^, We can readily obtain ruiotho? expression tor t6. wl.ich is often more
/ convenient than tliat just given. In Uiat I'ormuia we liave the expression
(5P/6T)e constant. Now. suppose tliat. instead of keeping « constant all
througli, we first allow the body to expand under constant tension ; if w is
the coefficient of linear expansion for tioat. and 3T the change in
temperature, the increase in the elongation is u)^~T ; now keep the
temperature constant, and diminish tJie tension until the shortening due
THERMAL EFFECTS ACCOMPANYING STRAINS.
133
fco the diminution in tension just compensates for the lengthening due to
the rise in temperatures. In order to diminish the elongation by wiJT we
must diminish the tension by qwoT where q is Young's modulus for the
wiie, hence
OP
hence by equation (1)
SP
aT
e coustant
= -qui
But qle is the additional tension SP required to produce the elongation he,
hence the increase in temperature Id produced by an increase of tension
2P is given by the equation
(2)
JKp
Equations (1) and (2) are due to Lord Kelvin.
Dr. Joule {Phil. Trans, cxlix. 1859, p. 91) has verified equation (2) by
experiments on cylindrical bai's of various substances, and the results of his
experiments are given in the following table. The changes in temperature
wei-e measured by thermo-electric couples inserted in the bars.
T
P
u
K
«P
5(9
observed.
59
calculated.
Iron .
Hard steel .
Cast iron .
Copper
286-3
274-7
282-3
274-2
7-5
7-0
6-04
8-95
1-24x10-5
1-23x10-5
1-11x10-5
1-7182x10-5
-110
-102
-120
-095
1-09 xlO»
1-09x109
1-10x109
1-08x109
- -1007
- -16-20
-•1481
--174
-•107
-•125
--115
- -154
A qualitative experiment can easily be tried with a piece of india-
rubber. If an indiarubber band be loaded sufficiently to produce a
considerable extension and if it be then warmed by bringing a hot body
near to it, it will contract and lift the weight ; hence the indiarubber gets
stiffer by a rise in temperature ; by the rule we have given, it ought to
increase in temperature when stretched, since by so doing it becomes
stift'er to resist stretching. That this is the case can easily be verified by
suddenly stretching a rubber-band and then testing its temperature by
placing it against a thermopile, or even between the lips, when it will be
found perceptibly warmer than it was before stretching.
We can easily calculate what efiect the heat produced will have on the
apparent elasticity if it is not allowed to escape. The modulus of elasticity,
when the change in strain takes place so rapidly that the heat has not
time to escape, is often called the adiabatic modulus.
Ratio of Adiabatic to Isothermal Elasticity.— Suppose we take
the case of a wire, and suppose the tension increased by ^P, if the heat
does not escape the increase ce in the elongation will be due to two causes
— one from the increase in the pull, the other from the increase in the
temperature. The first part is equal to hVjq, where q is Young's modulus
134-
PROPERTIES OF MATTER.
for steady strain ; the second part is equal to cdo> where ?0 is the change in
temperature, w the coeflScient of linear expansion ; lience
but by equation (2)
hence
ae
or
le
9
+ 10^6;
ao-
=r -
u.T„gP
JKp'
i =
1
JKp
^e
1
w-T^
hP
9
JKp
But if 2' is the adiabatic " Young's Modulus,"
~ q JKp
It follows from this equation that Ifq' is always less than Ifq or 7
(3)
is always greater than g, as we saw from general reasoning must be
^Ke^case! By equation p3) we can calculate the value of q'/q. The
results for temperature lo°C are given in the following table, taken from
Lord Kelvin's article on " Elasticity " in the Enct/clopcedia Bi'itannica :
Substance.
Zinc
Tin
Silver
Copper
Lead
Glass
Iron
Platinum
p
' K
7-008
•0927
7-404
-0514
10-369
•0557
8-933
•0949
11-215
•0293
2-942
•177
7-553
•1098
21-275
•0314
fa)
•0000249
•000022
•000019
■000018
•000029
•0000086
•000013
•0000086
7/ion
4
7
12
1
6
18
16
•56
■09
•22
•20
•74
-02
-24
-7
(flq deduced
from equat. 3.
_ -008
[•00362
•00315
. ^00325
: -00310
. -000600
[•00259
[•00129
Thus we see that in the case of metals q' is not so much as 1 per
cent, greater than q. In Wertheim's experiments, however, the excess
of q determined by acoustical methods over q determined by statical
methods exceeded in some cases 20 per cent. This discrepancy has never
been satisfactorily acco'inted for.
CHAPTER XIV.
CAPILLARITY.
Contents. — Surface Tension and Surface Energy — Rise of Liquid in a Capillary
Tube — Relation between Pressure and Curvature of a Surface — Stability of
Cylindrical Film — Attractions and Repulsions due to Surface Tension — Methods
of Measuring: Surface Tension — Temperature Coefficient of Surface Tension —
Cooling of Film on Stretching — Tension of very Thin Films — Vapour Pressure
over Curved Surface— Effects of Contamination of a Surface.
There are many phenomena which show that liquids behave as if they
were enclosed in a stretched membrane. Thus, if we take a piece of bent
wire with a flexible silk thread stretching from one side to the other and
dip it into a solution of soap and water so as to get the part between the
silk and the wire covered with a film of the liquid, the silk thread will be
drawn tight as in Fig. 90, just as it would be if the film were tightly
Fig. 90.
I'lG. i,i.
Fig. 92.
stretched and endeavouring to contract so that its area should be as smaR
as possible. Or if we take a framework with two threads and dip it into
the soap and water, both the threads will be pulled tight as in Fig. 91, the
liquid again behaving as if it were in a state of tension. If we take a
ring of wire with a liquid film upon it and then place on the film a closed
loop of silk and pierce the film inside the loop, the film outside will pull
the silk into a circle as in Fig. 92. The efiect is again just the same as it
would be if the films were in a state of tension trying to assume as small
an area as possible, for with a given circumference the circle is the curve
whii ii has the largest area ; thus, when the silk is dragged into the circular
form, tlie aTrrt of the film outside is as small as possible.
Another method of illustrating the tension in the skin of a liquid is
to watch the changes in shape of a drop of water forming quietly at the
end of a tube before it fi.nally breaks away. The observation is rendered
136
PROPERTIES OF MATTER.
much easier if the water drops are allowed to form in a mixture of
paraffin oil and bisulphide of carbon, as the drops are larger and form
more gradually. The shape of the drop at one stfige is shown in Fig. 93.
If we mount a thin indiarubber membrane on a hoop and suspend
Fio. 93.
Fio. 94.
it as in Fig. 94, and gradually fill the vessel with water and watch the
changes in the shape of the membrane, these will be found to correspond
closely to those in the drop of w^ater falling from the tube ; the stage
corresponding to that immediately preceding the falling away of the drop
is especially interesting ; a very marked waist forms in the membrane at
this stage, and the water in the bag falls rajiidl}^ and looks as if it were
going to burst away ; the
membrane, however,
reaches another figui-e of
equilibrium, and if no
more water is poured in
remains as in Fig. 94.
Again, liquids behave
as if the tension in their
outer layers was different
Fio. 95. for different liquids. This
may easily be shown by
covering a white flat-bottomed dish with a thin layer of coloured water
and then touching a part of its surface with a glass rod which has been
dipped in alcohol ; the liquid will move from the part touched, leaving the
white bottom of the dish dry. This shows that the tension of the water is
greater than that of the mixtuie of alcohol and water, the liquid being
dragged away from places where the tension is weak to places where it ia
strong.
CAPILLARITY.
137
VA.lvi
There is one very important difference between the behaviour of ordinaiy
stretched elastic membranes and that of liquid films, for while the tension
in a membrane increases with the amount of stretching, the tension in
a liquid film is independent of the stietching, provided that tliis is not so
great as to reduce^ the thickness of the film below about five millionths
of a centimetre. This can be shown by the following experiment : bend
a piece of wire into a closed plane curve and dip this into a solution of
soap and water so as to get it covered with a film, then hold the wire in
a nearly vertical position so as to allow the liquid in the film to drain
down ; this will cause the film to be thinner at the top than at the
bottom ; the difierence in thickness is very apparent when the film gets
thin enough to show the colours of thin plates, yet though the film is of
very uneven thickness the equilibrium of the film shows that the tension
is the same throughout,* for if the tension in
the thin part were greater than that in the
thick, the top of the film would di'ag the
bottom part up, while if the tension of the
thick part were greater than that of the thin
the lower part of the film would drag the top
part down.
Definition of Surface Tension.— Sup-
pose that we have a film stretched on the
framework ABOD, Fig. 96, of which the sides
AB, BC and AD are fixed while CD is
movable ; then, in order to keep CD in
equilibrium, a force F must be applied to it
at right angles to its length. This force is
required to balance the tensions exerted by
each face of the film ; if T is this tension,
then
2T.CD-F; Fig. 96.
the quantity T defined by this eqviation is called the surface tension of the
liquid ; for water at 18°C. it is about 73 dynes per centimetre.
Potential Energ-y of a Liquid arising- from Surface Tension. —
If we pull the bar CD out through a distance x, the Avork done is F.«, and
this is equal to the increase in the potential energy of the film, but
Fa? = 2T.CDa:; = Tx (increase of area of film). Thus the increase in the
potential energy of the film is equal to T multiplied by the increase in area,
so that in consequence of_surface tension a liquid will possess an amount of
potential energy equal to the product of the surface tension of the liquid and
the area of the surface. Starting from this result we can, as Gauss showed, y
deduce the consequences of the existence of surface tension from the I
principle that when a mechanical system is in equilibrium the potential J
energy is a minimum. Suppose that we take, as Plateau did, two liquids of
the same density, say^oil and a mixture of alcohol and water, and consider
the equilibrium of a mass of oil in the mixture. Since the density of the
oil is the same as that of the surrounding fluid, changes in the shape of the
mass will not affect the potential energy due to gravity ; the only change
* If the film is vertical the tension at the top is very slightly greater than that at
the bottom, so as to allow the difference of tension to balance the exceedingly small
weight of the film
138 PROPERTIES OF MATTER.
in the potential enei-gy will be the change in the energy dne to surface
tension, and, by the principle just stated, the oil will assume the shape iu
which this potential energy is a minimum — i.e., the shape in which the
area of the surface is a minimum. The sphere is the surface which for a
given volume has the smallest surface, so that the drops of oil in the liquid
will be spherical. This experiment can easily be tried, and the spherical
form of the drops is very evident, especially if the oil is made more
distinct by the addition of a little iodine.
If a drop of liquid is not surrounded by fluid of the same density,
but is like a drop of mercury on a plate which it does not wet, then any
change in the shape of the drop will affect the potential energy due to
gravitation as well as that due to surface tension, and the shape of the
drop will be determined by the condition that the total potential energy is
to be as small as possible ; if the drop is very large, the potential energy f
due to the surface tension is insignificant compared with that due to gravity,
and the drop spreads out
flat so as to get its centre of
gravity low, even though
this involves an increase in
the potential energy due to
the surface-tension. If, how-
ever, the drop is very small,
the potential energy due to gravity is insignificant in comparison with
that due to surface-tension, and the drop takes the shape in which the
potential energy due to surface-tension is as small as possible ; this shape,
as we have seen, is the spherical, and thus surface-tension will cause all
very small drops to be spherical. Dew-drops and rain-drops are very
conspicuous examples of this ; other examples are afforded by the
manufacture of spherical pellets by the fall of molten lead from a shot
tower and by the spherical form of soap-bubbles. We shall show later on
that if the volume of liquid in a drop is the same as that of a sphere of
radius a the liquid will i-emain very nearly spherical if a^ is small compai'ed
with T/gp where T is the surface-tension and p the density of the liquid.
Thus, in the case of water, where T is about 73, drops of less than 2 or 3
millimetres in radius, will be approximately spherical.
Another important problem which we can easily treat by the method of
energy is that of the spreading of one liquid over the surface of another.
Suppose, for example, we place a drop of liquid A on another liquid B
(Fig. 97), we want to know whether A will spread over B like oil over
water, or whether A will contract and gather itself up into a drop. The
condition that the potential energy is to be as small as possible shows that
A will spread over B if doing so involves a diminution in the potential
energy; while, if the spreading involves an inci "i^o in the potential
energy, A will do the reverse of r^ • ■,idir<j and will gath'.^r itself up in a
drop. Let us consider tl-e change in the potential eneigy due to an
increase S in the area of contact of A and B where A is a flat drop. We
have three surface-tensiri^" to consider: that of the surface of contact
between A and the air, which we shall call Tj ; that of the surface of
contact between B a'.d tne air, which we shall call T, ; and that of the
surface of contact of A and B, which we shall call T^^. Kow wnon we
increase the surface of contact between A and B by S we increase the
energy due to the surface-tension between these two fluids by Tj, x S, we
CAPILLARITY, 139
increase that due to the surface-tension between A and the air by T, x S
and diminish that due to the surface-tension between B and the air by
Tg X S. Hence the total increase in the potential energy is
<,7^ cLi and if this is negative S will increase — i.e., A will spread over B ; the con-
^ 1^1^, dition for this to be negative is that
so that if this condition is fulfilled the liquid A will spread out into a thin
film and cover B, and there will be no place where three Ii(]uid surfaces
meet. If, on the other hand, any one of the tensions is less than the sum
of the other two — i.e., if we can construct a triangle whose sides are
proportional to Tj, T^ and Tj^, then a drop of one liquid can exist on the
surface of the other, and we should have the three liquid surfaces meeting
at the edge of a drop. The triangle whose sides are proportional to
T„ Tj, T,2 is often called Neumann's triangle ; the experiments of
Quincke, Marangoni and Van Mensbrugghe, show that for all the liquids
hitherto investigated this triangle cannot be drawn, as one of the tensions
is always greater than the sum of the other two, and hence that there can
be no position of equilibrium in which three liquid surfaces meet.
Apparent exceptions to this are due to the fouling of the surface of one of
the liquids. Thus, when a drop of oil stands on water, the water surface
is really covered with a thin coating of oil which has spread over the
surface ; or again, when a drop of water stands on mercury, the mercury
surface is greasy, and the grease has spread over the water. Quincke has
shown that a drop of pure water will spread over the surface of pure
mercury.
Though three liquid surfaces cannot be in equilibrium when there is a
line along wHich all three meet, yet a solid and two liquid surfaces can be
in equilibrium ; this is shown by the equilibrium of water Or of mercury
in glass tubes when we have two fluids, water (or mercury), and air,
both in contact with the glass. The consideration of the condition of
equilibrium in this case naturally suggests the question as to whether
there is anything corresponding to surface-tension at the surface of
separation of two substances, one of which is a solid. Though in this case
the idea of a skin in a state of tension is not so easily conceivable as for a
liquid, yet there is another way of regarding surface-tension which is as
readily applicable to a solid as to a liquid. We have seen that the
existence of surface-tension implies the possession by each unit area of the
liquid of an amount of potential energy numerically equal to the surface-
tension : we may from this point of view regard surface-tension as surface
energy. There is no difficulty in conceiving that part of the energy of a
solid body may be proportional to its surface, and that in this sense the
body has a surface-tension, this tension being measured by the energy per
unit area of the surface.
Let us now consider the equilibrium of a liquid in contact with air and
both resting on a solid, and not acted upon by any forces except those due
to surface-tension. Suppose A, Fig. 98, represents the solid, B the liquid,
C the air, FG the surface of separation of liquid and air, ED the sur-
face of the solid. Let the angle FGD be denoted by Q ; this angle is
140
PROPERTIES OF MATTER.
called the angle of contact of the liquid with the solid. Let the surface
of separation FG come into the position F'G' parallel to FG. Then if FG
represented a position of equilibrium, the potential energy due to surface-
tension must be a minimum in this position, so that it will be unafi'ected
D
Fio. 98.
by any small displacement of the substances ; thus the potential energy
must not be altered by the displacement of FG to F'G'. This displace-
ment of the surface causes B to cover up a long strip of the solid, the
breadth of the strip being GG'. Let S be the area of this strip. Then
if Tj, Tj and Tj^ are respectively the surface-tensions between A and C, B
and 0, and A and B, the changes in the energy due to the displacement are :
(1) An increase Tj^S due to the increase S
in the surface between A and B.
(2) An increase T^S cos 0 due to the
increase S cos 0 in the surface between B
and C.
(3) A diminution T,S due to the diminu-
tion S in the surface between A and C.
Hence the total increase in the energy is
S(T,, + T,cos0-T,)
and as this must vanish when we have
equilibrium we have
T„-|-T, cos0 = T,;
or
T -T
cos 0 = ^ ^
T
Thus, if T, is greater than Tj^, cos 0 is
positive and 0 is less than a right angle ; if
Tj is less than Tjj, cos 0 is negative, and 0 is
greater than a right angle ; mercury is a
case of this kind, as for this substance 0 is
Fig. 9^. about 140°. The angle 0 is termed the
angle of contact. Since cos 0 cannot exceed
unity, the greater of the two quantities Tj or Tj^ must be less than the
sum of the other two. If this condition is not fulfilled the liquid B will
spread over the surface A.
Rise of a Liquid in a Capillary Tube. — We can apply the result we
have just obtained to find the elevation or depression of a liquid in a tube
which it does not wet and with which it has a finite angle of contact.
Suppose h is the height of the fluid in the tube above the horizontal
surface of the fluid outside, when there is equilibrium ; and suppose that
r is the radius of the tube at the top of the fluid column. Let T, be the
V = TT}*^ - -TTJ-''
2 , Trtj
3
hence A+-?' = — *
If 6 is greater tlian a right angle h is negative, that is, the level of the
liquid in the tube is lower than the horizontal surface ; this is strikingly
shown by mercury, but by no other fluid. The angle of contact between
mercury and glass was measured by Gay Lussac by causing mercury to
flow up into a spherical glass bulb ; when the mercury is in the lower part
of the bulb the surface near the glass will be very much curved ; as the
mercury rises higher in the bulb the curvature will get less ; the surface
of the mercury at different levels is represented by the dotted lines in
Fig. 100. There is a certain level at which the surface will be horizontal;
at this place the tangent plane to the sphere makes with a horizontal plane
an angle equal to the supplement of the angle of contact between mercury
and glass. A modification of this method is to make a piece of clean
r
CAPILLARITY. 141
surface-tension between the tube and air, T, that between the liquid and air
and Tjjthat between the tube and the liquid. Then, if there is equilibrium,
a slight displacement of the fluid up the tube will not alter the potential
energy. Suppose then that the fluid rises a short distance x in the tube,
thus covering an additional area ^ttvx of the tube, and diminishing the area
of the tube in contact with the air by tliis amount. This increases the
potential energy due to surface-tension by 2Trrx{T^^ — T,).
The increase in the potential energy due to gravity is the work done
(1) by lifting the mass td" x p x x, where p is the density of the liquid,
against gravity through a height^:^this is equal to gphirr^x ; and (2) by -t "*'*
lifting the volume?; of the meniscus through a height x — this work is equal
to (jpiw.
Hence the total increase in potential energy is
277-?-a;(T,j - T,) + gphnrx + gpvx^
and as this must vanish we have
;. + JL = 2(T,-T„),
irT' gpr
but if d is the angle of contact, we have just proved that
Tj cos 0 = T, - T„
, ,^v 2T.COS0
hence n + — - = — •
Trt" gpr
When the fluid wets the tube 6 is zero and cos 0 = 1. If the meniscus
is SO small that it may be regarded as bounded by a hemisphere, v is the
difference between the volume of a hemisphere and that of the circum-
scribing cylinder — i.e.,
142
TROPERTIES OF MATTER.
plate glass dipping into mercury rotate about a horizontal axis until the
surface of the meicury on one side of the plate is flat ; the angle made by
the glass plate with the horizontal is then the supplement of the angle of
*contact between mercury and glass.
The angle of contact between mercury and glass varies very widely
under different circumstances; thus the meniscus of the mercury in a
thermometer may not be the same when the mercury is rising as when it
is falling. We should expect this to be the case if tlie mercury fouls the
glass, for in this case the mercury when it falls is no longer in contact
with clean glass but with glass fouled by mercury, and we should expect
the angle of contact to be very different from that with pure glass. Quincke
found that the angle of contact of a drop of mercury on a glass plate
steadily diminished with the time; thus the angle of contact of a freshly
formed drop was 148'^ 55', and this steadily diminished, and after two days
Fig. 100.
Fig. 101.
was only 137° 14'; on taj)ping the plate the angle rose to 141° 19', and
after another two days fell to 140°.
If we force mercury iip a narrow capillary tube and then gradually
diminish the pressure, the mercury at first, instead of falling in the tube,
adjusts itself to the diminished pressure by altering the curvature of its
meniscus, and it is only when the fall of pressuie becomes too large for such
an adjustment to be possible that the mercui-y falls in the tube ; the con-
sequence is that the fall of the mercury, instead of being continuous, takes
place by a series of jumps. This effect is illustrated by the old experiment
of bending a piece of capillai-y tubing into a U-tube (Fig. 101), pouring
mercury into the tube until it covers the bend and stands at some height
in either leg of the tube ; if the tube is vertical, the mercury can be made
by tapping to stand at the same height in both legs of the tube. Now slowly
tilt the tube so as to cause the mercury to run up the left leg of the tube ;
if the tube is slowly brought back to the vertical, the mercury will be
found to stand at a higher level in the left leg of the tube than in the
right, while the meniscus will be flatter on the left than on the right.
Tliis principle explains the action of what are called Jamin's tubes, which
aie simply capillary tubes containing a large number of detached drops of
liquid ; these can stand an enormous difference of pressure between the
ends of the tube without any appreciable movement of the drops along the
CAPILLARITY.
143
tube. Thus, suppose that AB, CD, EF (Fig. 102) represent three consecu-
tive drops along the tube, then in consequence of the diflerent curvatures
A B
C D E F
FiQ. 102.
of AB at A and B the pressure in the air at A will be greater than that at B,
while the pressure at G will be greater than that at D, and so on ; thus
each drop transmits a smaller pressure than it receives ; if we have a largo
number of drops in the tube the difterence of pressure at the ends arising
in this way may amount to several atmospheres.
Relation between Pressure and Curvature of a Surface.— If
we have a curved liquid surface in a state of tension the pressure on the
concave side of the surface must be greater than that on the convex ; we
shall proceed to find the relation between the diflerence of pressure on the
two sides and the curvature of the surface.
Let the small portion of a liquid film, represented in Fig. 103 by ABCD
where AB and CD are equal and parallel and at right angles to AD and BO ,
be in equilibrium under the surface tension and a diflerence of pressure p
between the two sides of the film. When a system of forces acting on a
body are in equilibrium we know by Mechanics that the algebraical
sum of the work done by these forces when the body sufiers a small dis-
placement is zero. Let the film ABCD (Fig. 103) be displaced so that
each point of the film moves outwaid along the normal to its surface through
a small distance x, and let A'B'C'D' be the
displaced position of ABCD. Then the
work done by the pressure is equal to
p X area ABCD x x ;
the work done against the surface tension
is T X increase in area of the surface ; and
since a film has two sides the increase in
the area of the film is twice the difference
between the areas A'B'C'D' and the area
ABCD, Hence the work done against sur-
face tension is equal to
2T X (area A'B'C'D' - area ABCD)
Hence by the mechanical principle referred to
p X area ABCD xx = 2T(area A'B'C'D' - area ABCD)
if we are considering a drop of water instead of a film we musi write T
instead of 2T in this equation.
Spherical Soap-bubble. — In this case ABCD will be a portion of a
spherical surface and the normals AA', BB', CC, DD' will all pass through
O, the centre of the sphere. Let R be the radius of the sphere, then by
similar triangles
(1)
A'B' = AB^' = ABM +
OA
\
s)
B'C' = BC^' = Bc/n-^)
144
PROPERTIES OF MATTER.
The area A'B'C'D' = A'B'.B'C' = AB. Bc/n- ^Y
= AB.BC[1 + ^
'IX
as we suppose r/E- is so small that its square can be neglectecf.
Hence
Fia. 104.
area A'B'C'D'= area A BCD
Fio. 105.
(-S)
(2)
substituting this value for the area A'B'O'D' in equation (1)^ the equation
becomes
4T
so that the pressure inside a spherical soap-bubble exceeds the pressure
outside by an amount which is inversely proportional to the radius of the
bubble.
General Case of a Curved Soap-bubble.— If the element of tha
film ABCD forms a portion of a curved surface, we know from the theory
of such surfaces that we can find two lines AB, BC at right angles
to each other on the surface such that the normals to the surface
CAPILLARITY. 145
at A and B intersect in O, while those at B and 0 intersect
iu a point O'. The lines AB, BC are said to be elements of the
jurves of Principal Curvature of the surface, and AO and BO' are called
the Radii of principal curvature of the surface. We must now distinguish
between two classes of surfaces. In the first class, which includes spheres
and ellipsoids, the two points 0 and 0' are on the same side of the surface,
and the surfaces are called synclastic surfaces; in the second class, which
includes surfaces shaped like a saddle or a dice-box, O and 0' are on
opposite sides of the surface ; and the surfaces are called anti-clastic
surfaces. We shall consider these cases separately, and take first the
case of synclastic surfaces. In this case (Fig. 104) we have by similar
triangles
A'B' = AB— — - = ABn-|-— jifRifl the radius of principal curvature OA.
Similarly B'C = BCf 1 -^ ^ j if R' is the radius of principal curvature O'B.
Hence area A'B'C'D' = area ABCD^l +|^ i^'^^)
»areaABCD(l+.(^+^))
as we suppose tc/R, x/K both so small that we can neglect the product of
these quantities in comparison with their first powers. Substituting this
value for the area A'B'O'D' in equation (1) we get
^'^■.R
bk) <'>
Let us now take the case of an anti-clastic surface, represented in
Fig. 105. In this case we have
a'b'.ab(i + -)
hence area A'B'O'D' = area ABOd/i +a^/i - lA^
Substituting this value of the area A'B'CD' in equation (1) we get
We can include (3) and (4) in the general formula
if we make the convention that the radius of curvature is to be taken as
positive or negative according as the corresponding centre of curvatuie
a,
146
PROPERTIES OF MATTER.
is on the side of the surface where the pressure is grea'".esfe or on the
opp)site side.
When a soap film is exposed to equal pressures on the two sides 7) = 0,
and we must therefore have
K IV '
In this case the curvature in any normal section must be equal on 1 op{ o ite
to the curvature in the normal section at right angles to the first. By
Fio. 106.
stretching a film on a closed piece of wire and then bending the wire we
can get an infinite number of surfaces, all of which possess this property;
we can also get surface? with this property by forming a film between the
rims of two funnels open at the end, as in Fig. lOG. By moving the
funnels i-elati\ely to each other we get a most interesting series of
surfaces, all of which have their principal curvatures equal and opposite.
\
Tia. 107.
If the film is in the shape of a surface of revolution — i.e., one which can be
traced out by making a plane curve rotate about a line in its plane — we
know from the geometry of such surfaces that (Fig. 107)
E = PO
R' = PG
where 0 is the centre of curvature of the plane curve at P, and G the
point where the normal at P cuts the axis AG about -whidi the curve
rotates.
CAPILLARITY. U7
if the pressures on the two sides of the film are equal we must have
PO - - PG.
The only curve with this property is the catenary, the curve in which
a uniform heavy string hangs under gravity, and thirf, therefore, is the
shape of the cross-section of a soap film forming a surface symmetrical
about an axis, when the prf ssures on the two sides are equal.
Stability of Cylindrical Films.— Let us consider the case of a
symmetrical film whose surface approaches closely that of a right circular
cylinder. Let EPF be the curve which by its rotation about the straight
line AB generates the surface occupied by the film. EPF will not differ
much from a straight line, and PG, the normal at P, will be very nearly
J-
equal to PN Avhere PN is at right angles to AB. Hence, if R is the
radius of curvature at P and p the constant diti'erence of pressure between
the inside and outside of the film, we have
Let 9/ be the height of P above the straight line EF and a the distance
between the lines EF and AB, then
PN = a-f-2/
and as y is very small compared with a we have approximately
PJST a a^
Substituting this value of 1/PN in equation (1) we get
R 2T a a' a^['^^ [2T a) \ a' ^^
if y' is the distance of P from a horizontal line at a distance
below EF. Since the film is very nearly cylindrical, p is very nearly
equal to 2T/a, so that the distance between this line and EF will be
very small.
Hence we see from equation (2) that the reciprocal of the radius of
curvature at a point on the curve is proportional to the distance of the
point from a straight line. Now we saw (p. 96 ) that the path
a'
148
PROPERTIES OF MATTER.
described by a point fixed near to the centre of a circle when the circle
rolls on a straight line possesses this property, hence we conclude that the
cross-section of a nearly cylindrical film is a curve of this kind. The curve
possesses the following properties : it cuts the straight line, which is the path
of the centre of the circle, in a series of points separated by half the
circumference of the rolling circle, its greatest distance from this line
p
^^-
i
^ * -. »
M
L
Fia. 109,
is equal to the distance of the point from the centre of the rolling
circle, while the reciprocal of the radius of curvature at a point is pro-
portional to its distance from this line.
Let us now consider what is the pressure in a nearly cylindrical
bubble with a slight bulge. Let us suppose that the length of the bubble
is less than the distance between two points where the curve which
generates the surface crosses the path of the centre of the rolling
circle. The section of the bubble must form a part of this curve.
Let A and 0, Fig. 109, be the ends of the bubble APC, the
section of the film. Let the dotted line denote the completion of the
curve of which APC forms a part. Then if p is the excess of pressure
^'"-.
'' >
M
K
FlQ. 110.
inside the bubble over the outside pressure and P any point on the
curve,
'=-(^p^)
where p is the radius of curvature of the curve at P. Now if we take
P at Q, a point where the curve crosses its axis 1//3 = 0, hence
P=--
2T
CAPILLARITY.
149
Now if the film were straight between A and 0 the excess of pressure
/?' would be given by the equation
,_ 2T
^ AM*
As QK is less than AM, p is greater than p, hence the pressure in the
film which bulges out is greater than the pressure in the straight film.
We can prove in the same way that in a film that bends in, as in Fig. 110,
if the distance between the ends is less than the dibtance between the
^ ,-)'/ points Q and Q' on the curve , that is, if the length of the film is less than
C half the circumference of its ends, the pressure is less than the pressure
— ^-^T- \ in the straight film.
A • -,,. If the distance between the ends of the film is greater than half
^^ jA the circumference of the ends of the film these conditions are reversed.
t ^T^' ' For let Fig. 1 1 1 repre-
^ sent such a film bending
in ; as before, the excess of
pressure p will be given by
the equation
2T
P = .
fi
QK
where Q is the point where
the curve of the film crosses
its axis. If the film were
straight between A and C,
p', the excess of pressure,
would be given by the
equation
2T
^'"AM
f
-V — ~ V-
B
r
N
A
E
FiQ. 112,
Since in this case AM is greater than QK, p is less than p. Hence
the pressure in the film which bends in is greater than that in the
straight film. In a similar way we can prove that in this case the
pressure in a film which bulges out is less than the pressure in a straight
film. Hence we arrive at the result that, iTiheJen^h of_the ^Im is
less_than half the circumferenc_e of its end, the pressure_in afi^m
that bulges out ia' greater than thatjn_a_jlm which_bends in, while
150
PROPERTIES OF MATTER.
if the length ^f^the film is greater than its semi-circumference the
pressure^in the film that bulges put is less than the jpressure^in one
that bends in. Mr. Boys has devised a very beautiful experiment which
illustrates this point. The arrangement is represented in Fig. 112.
A and J3 are pieces of glass
tubing of equal diameter com-
municating with each other
through the tube C ; this com-
munication can be opened or
closed by turning the tap. E
and F are pieces of glass tubing
of the same diameter as Aj they
are placed vertically below A
and B respectively. The distance
between A and E and B and F
be altered by laising or
can
lowering the system ABC. First
begin with this distance less
than half the circumference of
the glass tube, Fig. 113, close
the tap and blow between A and
E a bubble which bulges out,
and between B and F, one that bends in. Now open the tap ; they will
both tend to straighten, air going from the one at A to help to fill up
that at B, showing that the pressure in the one at A is greater than ia
that at B. Now repeat the experiment after increasing the distance
between A and E and B and F to
more than half the circumference of
the tube. We now find on opening
the tap that the film which bulges
out is blown out still more, while the
one that bends in tends to shut itself
up, showing that air has gone from
B to A or that now the pressure at
B is greater than that at A.
It follows from this result jthat
the equilibrium of a cylindrical filin.
is unstable whenTitsTength is greater
tjian its circumference, while shorter
^ms.are stabled
For let us consider the equilibrium
of a cylindrical film between two
equal fixed discs, A and B, Fig. 115,
and consider the behaviour of a
movable disc C of the same size placed
between them. Suppose the length
of the film is less than its circum-
ference and that C is midway between A and B ; move C slightly towards
B, then the film between B and C will bulge out while that between A
and C will bend in. As the distance between each of the films is less than
half the circumference the pressure in the film which bulges out will be
greater than in that which bends in, thus C will be pushed back to its
Fig. 114.
CAPILLARITY.
151
c
Fio. 115.
original position and the equilibrium will be stable. If C is not midway
between AB but nearer to J3 than to A, then even if AC is greater than
the semi-circumference so that when C is pushed towards B the pressure
in AC is greater than when
the film is straight, yet it is
easy to prove that the excess
of pressure in BC is, in
consequence of its greater
curvature, greater than that
in AC, so that 0 is again
pushed back to its old posi-
tion and the film is again a.
stable.
Suppose now that the
distance between A and B is gi^eater than the circumference of the film,
and that C, originally midway between A and B, is slightly displaced
towards B. CB will bulge out and CA will bend in; as the length of
each of these films is gi^eater
than the semi-circumference
of the film the pressure in
BC will be less than that in
AC, and C will be pushed
still further from its original
position and the equilibrium
will be unstable. The film
will contract at one pait
and expand in another until
its two sides come into con-
tact and the film breaks up
into two separate spherical
portions.
These results apply to fluid
cylinders as well as to cylin-
drical films. Such cylinders
are unstable whentheir length
IS grea{er_than "tEeir circum-
ference. Examples of this
unstability are afibrded by the
breaking up of a liquid jet
into drops. The development
of inequalities in the thickness
of the jet is shown in Figs.
116 and 117 taken from instan-
taneous photogx*aphs. Thelittle ij'io. 116.
drops between the big ones
are made from the nari-ow necks which form before the jet finally
breaks up. Another instance of this instability is afforded by dipping
a glass fibre in water, the water gathers itself up into beads. A very
beautiful illustration of the same efiect is that of a wet spider's web,
shown in Fig. 118, when again the water gathers itself up into spherical
beads.
If the Auid is very viscous the effect of viscosity may counterbalance
152
PROPERTIES OF MArPER.
the instability due to surface tension ; thus it is possible to get long thin
threads of treacle or of molten glass
Force between two Plates
ntid quartz.
due to Surface-tension.— Let A
and 13 ( Fig. 11 'J) be two parallel plates
sepai-ated by a film of water or some
liquid which wets them; then, if d
is the distance between the plates
and D the diameter of the area of
the plate wet by the liquid, the
radii of curvature at the free sur-
face of the liquid are approximately
- d/2 and D/2, hence the pressure
inside the film is less than the
atmospheric pressure by
2T
Fig. 117.
---1
d DJ
or if cZ is very small compared with
D the difference of pressure is approximately
2T
Now the plate A is pressed towards B by the atmospheric pressure
and away from B by a pressure which is less than this by 2T{d ; hence, if
Fig. 118,
A is the area of the plate wet by the film, the force urging A towards
T^ o 2AT
B IS . , . .
d
The force varies inversely as the distance between the plates ; thus,
B
Fig. 119.
if a drop of water is placed between two plates of glass the plates are
forced together, and this still further increases the pull between the plates
as the area of the wetted sui-face increases while the distance between the
plates dimiuishos.
CAPILLARITY.
153
1
V
IV
0
s.
Attractions and Repulsions of small Floating: Bodies.— Small
bodies, such as straw or pieces of cork, floating on the surface of
a liquid often attract each other and cuUec^t together in clusters; this
occurs when the bodies are^all wet by the liquid, and also when^ione of
them are wet ;^ one body is wet and one is not wet they repel each other
when they come close together. To investigate the theory of this eflect,
let us suppose that A and B are two parallel vertical plates immersed in a
liquid which wets both of them, the liquid will stand at a higher level
between the plates than it does outside. We shall begin by showiBg that
the horizontal force exerted on a
plate by a meniscus such as PRQ, ^
UVW is the same as the force
which would be exerted if the u
meniscus were done away with and
the liquid continued horizontally
up to the surface of the plate. For
consider the water in the meniscus
PQR; it is in equilibrium under
I ; the horizontal tension at P, the
>A vertical tension at Q, the ^ force
exerted by the plate on the liquid,
'^' the vertical liquid pressure over
PR, and the' pressui-e of the atmo-
sphere over PQ. The resultant A
pressure of the atmosphere over
PQ, which we shall call tt, in the
horizontal direction is equal to the
pressure which would be exerted on
QR, the part of the plate wet by Fia. 120.
the meniscus, if this were exposed
directly to the atmospheric pressure without the intervention of the
liquid. The horizontal forces acting from left to right on the meniscus
^ «- — T- force exerted by plate on meniscus, j — "*=^ ->^<»x>-^-»^ \rrz,^
Since the meniscus is in equilibrium the horizontal forces must be in ^ilf-'
equilibrium ; hence ^. -
force exerted by meniscus on plate = T — tt,
but this is precisely the force which would be exerted if the meniscus were
done away with and the horizontal surface of the liquid prolonged to meet
the plate. Hence, as far as the horizontal forces are concerned, we may
suppose the surfaces of the liquid flat, and represented by the dotted lines
in Fig. 120. Considering now the forces acting on the plate A, the pulls
exerted by the surface-tension at R and U are equal and opposite ; on the left
the plate is acted on by the atmospheric pressure, on the right by the pressure
in the liquid. Now the pressure in the liquid at any point is less than the
atmospheric pressiu-e by an amount proportional to the height of the point
above the level of the undisturbed liquid ; thus the pressure on A tending
to push it towards B is greater than the pressure tending to push it away
from B, and thus the plates are pulled together.
Now suppose neither of the plates is wet by the liquid — a case repre-
154
PROPERTIES OP MATTER.
sented in Fig. 121. "We can prove, as before, that we may suppose the
fluid to be prolonged horizoutiilly to meet the plates. The force tending
to push the plate A towards 13 is the pressure in the liquid, the force
B
r-\
Tig. 121.
V
Fig. 122.
r~
tending to piish it away is the atmospheric pressure. Now the pressure
at any point in the liquid is greater than the atmospheric pressure by an
amount proportional to the depth of the point below the undisturbed
surface of the liquid ; hence, the pressure tending to push A to B will be
greater than that tending to push it away from
O 13, so that the plates will again appear to
attract each other.
Now take the case where one plate is wet
by the liquid while the other is not. The
section of the liquid surface will be as in Fig.
122, the curvature of the surface being of one
sign against one plate, and of the opposite sign
against the other. When the plates are a
considerable distance apait, the surfaces of the
liquid will be like that shown in Fig. 122;
between the plates there is a flat horizontal
surface at the same level as the undisturbed
liquid outside the plates ; in this case there is
evidently neither attraction nor repulsion between
Fio. 12a the plates. Now suppose the plates pushed
nearer together, this flat surface will diminish,
and the last trace of it will be a horizontal tangent crossing the liquid.
Since the curvature changes sign in passing from A to B, there must be a
place between A and B where it vanishes, and when the curvature
vanishes, the pressure in the liquid is equal to the atmospheric pressure ;
this point, at which the tangent crosses the surface, must be on the
prolongation of the free surface of the liquid. Now suppose that the
plates are so near together that this tangent ceases to bo horizontal, and
the liquid takes the shape shown in Fig. 123. We can show, by the
CAPILLARITY.
155
method given on p. 153, that the action on the plate A of the meniscus
inside A is the same as if the meniscus were removed and the liquid
surface stretched horizontally between the plates, the surface-tension in
this surface being equal to the horizontal comjJonent of the surface tension
at the point of inflection. Now consider the plate A ; it is pulled from
B by the surface-tension and towards it by only the horizontal component
of this. The force pulling it away is thus greater than the other, and the
plates will therefore I'epel each other. If the plates are pushed very near \
together so that the point of inflection on the surface gets suppressed the
liquid may rise between the plates and the repulsiou be replaced by an
attraction.
Methods of Measuring' Surface-tension.
By the Ascent of the Liquid in a Capillary Tube.— A finel>
divided glass scale is placed in a vertical position by means of a plumb
line, the lower end of the scale
dipping into a vessel V, which contains
some of the liquid whose surface
tension is to be determined. The
capillary tube is prepared by drawing
out a piece of carefully cleaned glass
tube until the internal diameter is
considerably less than a millimetre ; |V_y'
the bore of the tube should be as
uniform as possible, for although the
height to which the fluid rises in the
capillary tube depends only on the
radius of the tube at the top of the
meniscus, yet when we cut the tube
at this point to determine its radius,
if the tube is of uniform bore, no
error will ensue if we fail to cut it at
exactly the right place. Attach the
capillary tube to the scale by two
elastic bands, and have a good light
behind the scale. Dip the capillary
tube in the liquid, and it will rush
up the tube ; then raise the capillary
tube, keeping its end below the fluid
in V. This will make the meniscus
sink in the tube and ensure that the
tube above the meniscus is wetted by
the liquid. Now read off on the
scale the levels of the liquid in V
and the capillary tube, and the dif- Fig. 124.
erence of levels will give the height
to which the liquid rises in the tube. To measure r, the radius of the
tube atthe level of the meniscus, cut the capillary tube carefully across at
this point and then measure the internal radius by a good microscope with
a micrometer scale in the eyepiece. If the section, when observed in the
microscope, is found to be far from ciicular, the experiment should be
156
PROPERTIES OF MATTER.
repeated with another tube. The surface tension T is determined by the
equation (p. 141),
T = ip«( hr+ — ) where p is the density of the fluid.
If the angle of contact is not zero a knowledge of its value is required
before T can be determined by this method.
By the Measurements of Bubbles and Drops.— This method is
due to Quincke. The theory is as follows; suppose that A13, Figs. 125
Fia. 125.
and 126, represents the section of a large drop of meixury on a horizontal
glass plate or, when turned upside down a large bubble of air under a glass
plate in water. Let a central slab be cut out of the drop or bubble by two
parallel vertical planes unit distance apart, and suppose that this slab is
cut in half by a vertical plane at right angles to its length ; consider the
equilibrium of the portion of this slab above the horizontal section BC of
gi-eatest area in the case of the drop, and below it in the case of the bubble.
Fig. 126.
The horizontal forces acting on the upper portion are the surface tension
T, and the horizontal pressures acting over the flat section ADEC and the
curved surface. If the drop is so large that the top may be considered as
plane there will be no change of pressure as we pass from the air just above
the surface of the drop to the mercury just below it ; * in this case the
difference in the horizontal components of the pressure over ADEC and
the pressure of the atmosphere over the curved surface is, since AD is
unity, equal to v ^x^«^...u«_ _ Pi hi
ypT>W
i^^\-
>\.j-i-a ^'-'^
b£./H^.f^^
As this must be balanced by the surface tension over AD we must have
T = ypJ)W (1)
By considering the equilibrium of the portion ABFGHD of the drop we
have T(l + cos w) - igph' (2)
where h is the thickness of the bubble or drop, and w the angle of contact
at F between the liquid and the plate. From equation (2) we have
• If the drops are not large enough for this assumption to be true, a correction
has to be applied to allow for the difference in pressure on the two sides of the
surface through A.
CAPILLARITY.
157
4Tcos»-
h? =
99
Thus the thickness of all large drops or bubbles in a liquid is independent of
tlie size of the drops or bubbles. By measuring either DE or h, and using
equation (1) or (2) we can determine T. In the case of bubbles it is more
convenient to use, instead of a flat piece of glass, the concave surface of a
large lens, as this facilitates greatly the manipulation of the bubble. In
this case, if we use equation (2), we must remember that h is the depth of the
bottom of the bubble below the horizontal plane through the circle of
contact of the liquid with the glass. Thus, in Fig. 127, A is equal to NE and
not to AE. It is more convenient to measure AE and then to calculate NE
from the radius of curvature of the lens and the radius of the circle of
contact of the glass and the liquid. Determinations of the surface tension
N
E
Fig. 127.
of liquids by this method have been made by Quincke, Magie, and Wilbei-
f orce.* Magie used this method to determine the angle of contact, as it is
evident from equations (1) and (2) that
(t) h
cos- = -=
2 ^/2DE
By this method Magie {Phil. Mag., vol. xxvi.
following values for the angle of contact with glass :
1888) found the
Angle zero.
Ethyl alcohol .
Methyl alcohol
Chloroform
Formic acid
Benzine .
Angle finite.
Water (?)
Acetic acid
Turpentine
Petroleum
Ether .
u
small
20°
17°
26°
16°
Determination of the Surface-tension by Means of Ripples.—
The velocity with which waves travel over the surface of a liquid depends
on the surface-tension of the liquid. The relation between the velocity and
surface-tension may be found as follows : Let Fig. 128 represent the section
of a harmonic wave on the surface of the liquid, the undisturbed level of
the liquid being xy. If gravity were the only force acting, the increase in
vertical pressure at N due to the disturbance produced by the wave would
be equal to gpP^, when p is the density of the liquid.
The surface tension will give rise to an additional normal, and therefore
T
approximately vertical, pressure equal per unit area to :g , where II is the
* See foot-note on opposite page.
il
^'^^^-'^
/?'
i58
PROPERTIES OF MATTER.
radius of curvature of the section of the wave by the plane of the paper;
the radius of curvature in the normal plane at right angles to the plane of
the paper is infinite. Now if the amplitude of the wave is very small
compared with the wa\'e lenirth, the wave curve may be generated by a
point fixed to a circle rolling m a straight line ; the amplitude is equal ,
to the distance of the point from the centre of the circle, and the
P
Fio. 128.
wave length is equal to the circumference of the rolling circle. The line
xy is the path of the centre of the rolling circle, Now we saw (^p 9G) that
for such a curve
R a-
where a is the radius of the rolling circle ; but if X is the wave length
27ra = X, so that
1 _47r^PN
R X^
Thus the pressure at N, due both to gravity and surface-tension, is
hence we see that the effects of surface-tension are the same as if gravity
were increased by 47r-T/X-p. Now the velocity of a gravity wave on deep
water is the velocity a body would acquire under gravity by falling
vertically through a distance X/47r, where X is the wave length— i.e., the
velocity is JgX/'Jn. Hence v, the velocity of a wave propagated under
the influence of surface-tension as well as gravity, is given by the equation
The velocity of propagation of the wave is thus infinite both when
the^jvave length is zero and when it is infinite ; it is proportional toThe
square root of an expression consisting of the sum of two terms whose
product is constant. It follows from a well-known theorem in algebra
that the expression will be a minimum when the two terms are equal.
Thus the velocitj^f propagation of the^ waves wjUbe least when
4,r-T
9-
X-t
or when
= 27r\/-
in this case the velocity is equal to
;x
CAPILLARITY.
159
In the case of water, for which T = 75,
X = 1'7 cm., and v = 23 cm. /sec.
Fig. 129.
Hence no waves can travel over the surface of water with a smaller
velocity than 23 cm. per second. For any velocity greater than this it
is possible to find a wave length X such that waves of this length will
travel with the given velocity. Waves whose lengths are smaller than
that corresponding to the minimum velocity are called "ripples," those
whose lengths exceed this value " waves." A wave is propagated chiefly
by gravity, a ripple chiefly by surface tension.
The velocity of a '• wave " increases as the wave length increases, while
that of a " ripple " diminishes. Interesting examples of the formation
of ripples are furnished by the standing patterns often seen on the surface
of running water near an obstacle, such as a
stone or a fishing-line. Thus, let AB represent
a stone in a stream running from right to left,
the disturbance caused by the flow of the water
against the stone will give rise to ripples which
travel up stream with a velocity depending upon
their wave length. Close to the stone the
velocity of the water is zero, so that the ripples
travel rapidly away from the stone. When,
hov^^ever, we get so far away from the stone, say
at P, that the velocity of the water is greater
than 23 cm. /sec, it is possible to find a ripple of
such a wave length that its velocity of propagation
over the water is equal to the velocity of the
stream, the ripple will be stationary at P, and will form there a pattern of
crests and hollows. As the velocity of the water increases as we recede
from the stone the ripples which appear stationary must get shorter and
shorter in wave length, and thus the crests in the pattern will get neai-er
and nearer together as we proceed up stream. We see that the condition
that the pattern should be formed at all is that the velocity of the stream
must exceed 23 cm. /sec. Fig. 129 is taken from a photograph of the
ripples behind a stone in running water. A similar explanation applies to
the pattern in front of a body moving through the liquid.
Lord Rayleigh was the first (Phil. Mag., xxx. p. 38G) successfully to
apply the measurement of ripples to the determination of the surface-
tension, and his method was used by Dr. Dorsey {Phil. Mag., xliv. p. 3G9)
to determine the surface-tension of a large number of solutions. Lord
Rayleigh's method is to generate the ripples by the motion of a glass plate
attached to the lower prong of an electrically driven tuning-fork, and
dipping into the liquid to be examined. To render the ripples (which for
the theory to apply have to be of very small amplitude) visible, light reflected
from the surface is brought to a focus near the eye of the observer. On
account of the rapidity with which all phases of the waves are presented
in succession it is necessary, in order to see the waves distinctly, to use
intermittent illumination, the period of the illumination being the same
as that of the waves. The illumination can be made intermittent by placing
in front of the source of light a piece of tin plate rigidly attached to the
prong of a tuning-fork, acd so arranged that once on each vibration the
160 PROPERTIES OF MATTER.
li<yht is intercepted by the interposition of the plate. This fork is
in unison with the one dipping into the liquid. It is driven electro-
magnetically, and the intermittent current furnished by this fork is
used to excite the vibrations of the dipping fork. By this means the
ripples can be distinctly seen, the number between two points at a known
distance apart counted, and the wave-length X determined. If r is the
time of vibration of the fork vt = \,
and since <^ = K- + ^r—
T_ X^ _g\*
p ~ 2^ 47r*
an equation from which T can be determined. The second term in this
expression is in these experiments small compared with the first.
Determination of Surface Tension by Oscillations of a
Spherical Drop of Liquid. — When the drop is in equilibrium under
surface-tension it is spherical ; if it is slightly deformed, so as to assume
any other form, and then left to itself, the surface-tension will pull it
back until it again becomes spherical. When it has reached this state
the liquid in the drop is moving, and its inertia will carry the drop through
the spherical form. It will continue to depart from this form until the
surface-tension is able to overcome the inertia, when it is again pulled back
to the spherical form, passes through it and again returns ; the drop will
thus vibrate about the spherical shape. We can find how the time of
vibration depends upon the size of the drop by the method of dimensions,
and the problem forms an excellent example of the use of this method.
Suppose the drop free from the action of gravity, then t, the time of
vibration of the drop, may depend upon a the radius, p the density, and
S the surface-tension of the liquid ; let
« = CaVS^
where 0 is a numerical constant not depending upon the units of mass,
length, or time. The dimensions of the left-hand side are one in time,
none in length, and none in mass, which, adopting the usual notation, we
denote by [T]^ [L]" [M]" ; the right-hand side must therefore be of the
same dimensions. Now a is of dimensions [T]« [L]' [M]" ; p, [T]" [L]-^ [Mji ;
and S, since it is energy per unit area, [T]-^ [L]" [M]^ ; hence the dimen-
sions of aY^' are, [T]"-' [L]-^^+'' [M]-+^. As this is to be of the dimensions
of a time, we have
-22 = 1, -3y + x = 0, y + z = 0
therefore x = ^, y = ^, z= -|
So that t, the time of vibration, varies as Vpa'ys ; i.e., it varies as the
square root of the mass of the drop divided by the surface-tension; a more
complete investigation, involving considerable mathematical analysis, shows
that t = -^/y P ^ where t is the time of the gravest vibration of the drop.
The reader can easily calculate the time of vibration of a drop of any size
if he remembers that the time of vibration of a drop of water 25 cm. in
radius is very nearly 1 second. The vibrations of a sphere under surface-
CAPILLARITY.
161
tension can easily be followed by the eye if a large spherical drop of water
is formed in a mixture of petroleum and bisulphide of carbon of the same
density. Lenard (Wiedemann's Annalen, xxx. p. 209) applied the
oscillation of a drop to detei-mine the surface-tension of a liquid. He
determined the time of vibration by taking instantaneous photographs of
the drops, and from this time deduced the surface-tension by the aid of
the preceding formuhe.
Determination of Surface-tension by the Size of Drops.— The
surface-tension is sometimes measured by determining the weight of a drop
of the liquid falling from a tube. If we treat the problem as a statical
one and suppose that the liquid wets the tube from which it falls, then
just on the point of falling the drop below the section ^i5 (Fig. 130) is to be
regarded as in equilibiium under the surface-tension acting
upwards, the weight of the drop acting downwards, the
pressure of the air on the surface of the drop acting upwards,
and the pressure in the liquid acting downwards across the
gection AB. If a is the radius of the tube, T the surface-
tension, then the upward pull is 2naT. If we suppose at
the instant of falling that the drop is cylindrical at the end of
the tube, the pressure in the liquid inside the drop will be
greater than the atmospheric pressure by_T/a (see p. 145),
Hence the effect of the atmospheric pressure over the surface
of the drop and the fluid pi-essure across the section AB is a
downwards force equal to iraP'Tja or TraT. Hence, if w is the weight of
the drop we have, equating the upwards and downwards forces,
27raT = to + iraT ; or TraT = w.
The detachment of the drop is, however, essentially a dynamical pheno-
menon, and no statical treatment of it can be complete. We should not
therefore expect the preceding expression to accord exactly with the results
of experiment. Lord Eayleigh* finds the relation 3-8aT = to to be sufficiently
exact for many purposes. Most observers who have used this method
seem to have adopted the relation 27raT = tw, a formula which gives little
more than half the true surface-tension ; the error comes in by neglecting
the change of pressure inside the drop produced by the curvature of its
surface.
Wilhelmy's Method.t— This consists in measuring the downward pull
exerted by a liquid on a thin plate of glass or metal partly immersed in the
liquid ; the liquid is supposed to wet the plate. The pull can be readily
measured by suspending the plate from one of the arms of the balance and
observing the additional weight which must be placed in the other scale-pan
to balance the pull on the plate when it is partially immersed in the liquid,
allowance being made if necessary for the effect of the water displaced. If
I is the length of the water-line on the plate, T the surface-tension, then i!
the liquid wets the plate the downward pull due to surface-tension is T^.
Method of Detachment of a Plate.-— Some observers have deter-
mined the surface-tension of liquids by measuring the pull required to drag
a plate of known area away from the surface. The theory of this method
resembles in many respects that by which we determined the thickness of
^ drop or air bubble {see p. 156). Let us take the case of a rectangular
* Lord Rayleigh, Phil. Mag., 48, p. 321.
t Glazebrook and Shaw, Practical Physics, oh. vii. § X. L
7'/-
ktcr^
162 PROPERTIES OF MATTER.
plate being pulled away from the surface, and let the figure represent a
section by a plane at right angles to the length of the rectangle. Considering
the equilibrium of the portion whose section is EBCF, and whose length
perpendicular to the paper is unity, the horizontal forces acting upon it
are : (1) the forces due to surface-tension— i.e., 2T acting from left to right ;
(2) the atmospheric pressure on the curved surface BG acting from right to
left, which is equal to Tld
J? n where 11 is the atmos-
pheric pressure and d is
the height of the lower
■j? ^ surface of the plate above
Tig. 131. the undisturbed level of
the liquid ; and (3) the
fluid pressure acting across the surface EF from left to right. The
pi-essure in the liquid at F i?, equal to IT, and therefore the resultant fluid
pressure across EF is equal to Hd-^gpd', where p is the density of the,
liquid. Hence, equating the components in the two directions, we have "^^^'^f
2T + ncZ - lopd' = Ud, ordr^ = ~ ^
ffP
Now the fluid pressure just below the surface is less than the atmospheric
pressure by gpd, hence the upward pull P required to detach an area of the
plate equal to A is equal to Agpd, and substituting for d its value, we find
p = 2aVi>7
Jaegfer's Method. — In this method the least pressure which will force
bubbles of air from the narrowjorifice ofa'capillary tube dipping into_the
n^mdlsjmeasured. The pressure ina spherical cavity exceeds the pressure
outsidenoy"2T7a~where a is the radius of the sphere, hence the pressure
required to detach the bubble of air exceeds the hydrostatic pressure at the
orifice of the tube by a quantity proportional to the surface-tension. This
method, which was used by Jaeger, is a very good one when relative and
not absolute values of the surface-tension are required ; when, for example,
we want to find the variation of surface-tension with temperature.
The following are the values of the suiface-tension at 0° C, and the
temperature coefficients of the surface-tension for some liquids of frequent
occurrence. The surface-tension at t° 0. is supposed to be equal to T^ - fit.
. "lly
. -087
. -132
. -379
. -152
The surface-tension of salt solutions is generally greater than that of
pure water. If T„ is the surface-tension of a solution containing n gramme
equivalents per litre, T„ the surface-tension of pure water at the same
temperature, Dorsey* has shown that T„ = T^. + lxn, where R lias the
following values— NaCl (1-53); KCl (1-71); h{Nsi.jGO^) (200); i(K,CO^
(1-77); ](ZnS0J(l-8G).
♦ Dorsej, Phil. Mag., 44, 1897, p. 369.
Liquid
Ether (C,H,„0)
Alcohol (C,H,0) .
Benzene (CgHg)
To
. 19-3
. 25-3
. 30-6
Mercury .
Water .
. 527-2
. 75-8
CAPILLARITY. l63
On the Effect of Temperature on the Surface-tension of
LiQ,uids. — The surface-tension of all liquids diminishes as the temperature
increases. This can be shown in the case of water by the following
experiment : A pool of water is formed on a horizontal plate of clean
metal ; powdered sulphur is dusted over the surface of the water and heat
applied locally to the under surface of the metal by a fine jet. On the
application of the heat the portion of the water immediately over the flame is
rapidly swept clear of the sulphur ; this is due to the greater tension in
the cold liquid outside pulling the sulphur away against the feebler tension
in the warmer water.
Eotvos {Wied. Ann. 27, p. 448) has pointed out that for many liquids
d{Tv^)/dl is equal tu- 2'1, being independent of tlie nature of the liquid and
lEi tem2)erature; here T is the sni-face-tension of the liquid, v the "molecular
\ volume" — i.e., the molecular weight divided by the density — and t the
temperature. It is clear that, if we assume that d{Tv^)ldt has this value
for a liquid whose density and surface-tension at difterent temperatures
are known, we can determine the molecular weight of the liquid. The
^ method has been applied for this purpose, and some interestmg results
have been obtained ; for example, water is a liquid for which Eotvos' rule
does not hold, if we suppose the molecular weight of water to be 18.
If, however, we assume the molecular weight of water to be 36 — i.e., that
each molecule of water has the composition 2II2O, then Eotvos' rule is
found to hold at temperatures between 100° and 200° 0. ; below the lower
of these temperatures the molecular weight would have to be taken as
greater than 3G in order to make Eotvos' rule apply. Hence, Eotvos con-
cluded that the molecules of water, or at any rate the molecules of the
surface layers, have the composition 211,0 above 100° C, while below that
temperature they have a still more complicated composition.
It follows that if Eotvos' rule is true,
Tv3 = 2-1 {t,-t)
where ^j is some constant temperature, which can be determined if we
know the value of T and v at any one temperature ; t^ is the temperature at
which thfi siyfapft-t.pnsinT^ vfinishegj it is therefore a temperature which
probably does not difler much from the critical temperature; the values of
i, for ether, alcohol, water^ are roughly about 180°, 295", 560° 0. Their
critical temperatures are estimated by Van der Waals to be 190°, 256°,
390° C.
Cooling due to the Stretching' of a Film.— Since the surface-
tension changes with the temperature, any changes in the area of a film will,
as they involve work done by or against surface-tension, be accompanied by
thermal changes. We can calculate the amount of these thermal changes
if we can imagine a little heat engine which works by the change of
surface-tension with temperature. A very simple engine of this kind is as
follows : Suppose that we have a rectangular framework on which a film
is stretched, and that one of the sides of the framework can move at right
angles to its length. Let the mass of the framework and film be so small
that it has no appreciable heat capacity. Suppose we have a hot chamber
and a cold chamber, maintained respectively at the absolute temperatures
0, and d^, where 0, and d.^ are so near together that the amount of heat
I'equired to raise the body from 6.^ to B^ is small compared with the
thermal eflect due to change of area Let us place the film in the hot
164 PROPERTIES OF MATTER.
chamber, and stretch it so that its area increases by A, then take it out
of the hot chamber and place it in the cold one, and allow the film to
contract by the amount A ; the film has thus recovered its original area.
Let it be now placed again in the hot chamber. If the surface-tension of
the film when in the cold chamber is greater than when in the hot, then
the film when contracting may be made to do more work than was
required to stretch it, so that there will be a gain of work on the cycle ;
the process is plainly reversible, so that the film and its framework and
the two chambers constitute a reversible engine. Hence, if Hj is the
heat absorbed in the hot chamber, H^ that given out in the cold, both
being measured in mechanical units, we have by the Second Law of
Thermodynamics,
5] = 5? = ^^1 ~ ^» (1)
0j 03 0, - f>3
If Tgj, Tg., are respectively the surface-tensions at the temperatures 6,
and 02, then the work done in stretching the film = 2T0^A, while the work
done by the film when conti^acting is 2Te2A, hence the mechanical work
gained = 2(Te,-T0j) A. By the principle of the Conservation of Eoergy
the mechanical work gained must equal the difference between the
mechanical equivalents of the heat taken from the hot chamber and given
up to the cold ; hence
H,-H, = 2(T,,-T,0A
and from (1) H, = 2d,A^^^^^^
0j 0j
If /3 is the temperature coefiicient of T, then
/3 = '
1 _ T^i - Tg
6,-0,
hence H,= -20,A/3
Thus Hj is positive when j3 is negative, so that when the surface-
=> \j,<^ -vv^ tension gets less as the temperature increases, heat must be applied to the
^ film to keep the temperatvu-e constant when it is extended — i.e., the_film
ilJLaft to itself will cool wlien_jDulled_oiit. This is an example of the rule
given on page 1^2THat the temperature change which takes place is such
\!! as to make the system stifl'er to resist extension. For water /3 is about
> -^' f T/550, so rhat the mechanical equivalent of the heat required to keep
the temperature constant is about half the woi^k done in stretching
the film.
Surface-tension of very thin Films.— The fact that a vertical
soap film when allowed to drain shows different colours at different
places and is yet in equilibrium shows that tho^ thickness of the film
may vary within wide limits without any subsbmtial change in the
euifnce-tension. The connection between the thickness of the fifm
ana tlie surtace-tension was investigated by llucker and Reinold.* The
method used is represented diagrammatically in Fig. 132. Two cylindrical
films were balanced against each other, and one of them was kept thick by
passing an electric current up it ; this keeps the film from draining, the
* JUicker and Reinold, Phil. Trans. 177. part ii. p. 627, 1886.
CAPILLARITY.
16*5
L.i.
1
other film was allowed to drain, and a difference of surface-tension was
indicated by a bulging of one of the cylinders and a shrivelling of the
other. When films are fiist formed the value of their surface-tension is
very irregular ; but lliicker and Reinold found that, if they were allowed
to get into a steady state, then a direct comparison of the surface-tension
overarange of thickness extending from ISoOyu.yii {j-i.jx is 10"" cm.) down to
the stage of extreme tenuity, when the film shows the black of the first order
of Newton's scale of colour,
showed DO appreciable
change in surface-tension,
althougli, had the ditlerence
amounted to as much as I ^ j>- U
one- half per cent., Reinold
and Riicker believed they
could have detected it. A
large number of determina-
tions of the thickness of
the black films were made,
some by determining the
electrical i-esistance and
then deducing the thick-
ness, on the assumption
that the specific resistance
is the same as for the
T
7T
i
%
_y
*
"A
B
V
A
liquid in bulk, others by Fig. 132.
determining the retarda-
tion which a beam of light suffers on passing through the film, and
assuming the refraction index to be that of the liquid in mass : all these
determinations gave for the thickness of the black films a constant value
a^out^2 n-ii. At first sight it appears as if the surface-tension suffered
no^ change until the thickness is less than 12 /x.yu. The authors have
shown, however, that this is not the right interpretation of their results,
for they find that the black and coloured parts of the film are separated
by a sharp line showing that there is a discontinuity in the thickness.
In extreme cases the rest of the film may be as much as 250 times thicker
than the black part with which it is in
contact. The section of a film showing r [~ |
a black part is of the kind shown in
Fig. 133. The stability of the film Fig. 133.
shows that the tension in the thin
part is equal to that in the thick. It is remarkable that in these films
there are never any parts of the film with a thickness anywhere between
12 yu./i. and something between 45 and 95 fx.fi.; films whose thicknesses
are within this range are unstable. This is what would occur if the
surface-tension first begins to diminish at the upper limit of the unstable
thickness, and after diminishing for some time, then begins to increase as
the thickness of the film gets less, until at 12 ^.^. it has regained its
original value ; after this it increases for some time, and then diminishes
indefinitely as the thickness of the film gets smaller and smaller. The
changes in surface-tension are represented graphically by the curve in
Fig. 134, where the ordinates represent the surface-tension and the
libscissae the thickness of the film. For suppose we have ft film thinning, it
■S
166 PROPERTIES OP MATTER.
will be in equilibrium until the upper part gets the thickness corresponding
to the point P on the curve ; as the tension now gets less than in tlie thicker
part of the film, the thicker parts pull the thin part away, and would cei'tainly
break it, were it not that alter the film gets thinner than at R the tension in-
creases until, wlien the film reaches the thickness corresponding to Q, the
tension is the same as in the thick film, and there is equilibrium between the
thick and the thin pieces of the film. This equilibrium would be stable,
for if the film were to get thinner the tension would get greater, and the
film would contract and thicken again, while if it got thicker the tension
would fall and the film would be pulled out until it regained its original
thickness. Thus all the films which are in contact with thick films must
have the constant "tluckness corresponding to (J. The equilibrium at W,
when the tension has the same value as at Q, is unstable, for any
extension of the film lowers the tension, and thus makes the film yield
more readily to the extension. The region between R and P is unstable,
^ Thickness
Fig. 134.
SO is that between T an^J2^ The region TR would be stable, but would
loe very difficult to realise. If we start with a thick film and allow it to
thin, the only films of thickness less than that at P which will endure will
be those whose thickne.S3 is constant and equal to the thickness at Q.
Johannot (Phil. Mag., 47, p. 501, 1899) has recently shown that a black
film of oleate of soda may consist of two portions, one having a thickne.ss
of 12 f^i.^, the other of 6 ^i./i. In this case there mu.st bs another dip
between S and R in the curve representing the relation between surface-
tension and thickne.ss.
Vapour Pressure over a Curved Surface. — Lord Kelvin was the
first to show that in consequence of suiface-tenision the vapour pressure in
equilibrium with a curved surface is not the same as the pressure of the
vapour in equilibrium with a flat one. We can see from very genei-al
considerations that this must be the case, for when water evaporates from
a flat surface there is no change in the area of the surface and therefore
no change in the potential energy due to surface-tension ; in the case of a
curved surface, however, such as a spheric;il diop, when water evaporates
there will be a diminution in the area of the surface and therefore a
Capillarity.
167
1
dimihtition in tlie potential energy due to surface-tension. Thus the
surface-^tension will promote evaporation in this case, aa evaporation is '-i H
accompanied by a diiuinuticni iu the potential enern;3\ Thus evaporation ^
will go on further from a spherical drop than from a plane surface ; that is,
thepressure of the water vapour in equilibrium with the spherical drop is
greater than for the plane area. "
Lord Kelvin's determination of the effect of curvature on the vapour
pressure is as follows : Let a fine capillary
tube be placed in a liquid, let the liquid rise
to A in the tube, and let B be the level of the
liquid in the outer vessel. Then there must
be a state of equilibrium between the liqiiid
and its vapour both at A and B, otherwise
evaporation or condensation would go on and
the system would not attain a steady state.
Let p p be the pressures of the vapour of the
liquid at B and A respectively, h the height
of A above B,
p=p' + pressure aue to a column of vapour
whose height is h
^p + gah,
(1)
where a is the density of the vapour. If r is
the radius of the surface of the liquid at A,
then T being the surface-tension,
2T ca difference of pressure on the two sides of
r the meniscus.
Now the pressure on the liquid side of the
meniscus is equal to 11 - gph where p is the
density of the liquid and 11 the pressure at
the level of the liquid surface in the outer
vessel ; the pressure on the vapour side of the meniscus is 11 - gah ; thus
the difference of pressxu-es is equal to g[p — a)h, so that
— = 9{p-<^V^*
r
FiQ. 135.
or
gah =
2T
Hence by equation (1)
p =p-
r p - ff
2T <T
r
t
— a
* In the investigation of the capillary ascent in tubes given on p. Ill, c is neglected
in comparison with p.
f The formula in the text gives the value for^'-^ when this is small compared
with p ; the general equation for p' may be proved to be (neglecting a in comparison
with p) ^ P' - 2T. 1
log^ = —
P
R^
where 9 is the absolute temperature and R the constant in the equation for a perfect
gas — i.e., pv = ^Q.
l68
PROPERTIES OF MATTER.
hence the equilibrium vapour pressure over the concave hemispherical
surface is less than that over a plane surface at the same temperature by
2T<r/(f) - (T)r. We may write this as io(T/{p — a) where w is the amount by
which the pressure below the curved surface is less than that below the plane.
If the shape of the liquid surface had been convex, like that of a dewdrop,
instead of concave, the pressure below the curved surface of liquid would be
greater than that in the plane sui face instead of being less, and the pressure
of the water vapour over the surface would be greater than that over a plane
surface. It can be shown that if an external pressure w were applied to a plane
— >.
is
n-
Fio. 136.
surface the vapour pressure would be increased by wa/p (see J. J. Thomson,
Applications of Dynamics p. 171). Unless the drops are exceedingly small,
the effect of curvature on tl>e vapour pressure is inappreciable ; thus if the
radius of the drop of water is one-thousandth part of a millimetre the
change in the vapour pressure only amounts to about one part in nine
hundred. As the effect is inversely proportional to the radius, it in-
creases rapidly as the size of the drop diminishes, and for a drop 1 yu./i
in radius the vapour pressure over the drop when in equilibrium would be
more than double that over a plane surface. Thus a drop of this size
would evaporate rapidly in an atmosphere from which water would condense
on a plane surface. This has a very important connection with the
phenomena attending the formation of rain and fog by the precipitation of
water vapour. Suppose that a drop of water "had to grow from an
indefinitely small drop by pi^ecipitation of water vapour on its surface;
since the vapour pressure in CLjuilibrium with a very small drop is much
CAPILLARITY. 169
greater than the normal, the drop, unless placed in a space in which the
water vapour is in a very supersaturated condition, will evaporate and
diminish in size instead of being the seat of condensation and increasing in
radius. Thus these small drops would be unstable and would qtiiclcly
disappear. Hence it would seem as if this would be an insuperable difficulty
to the formation of drops of rain or cloud if these drops have to pass
through an initial stage in which tlieir size is very small. Aitken has
shown that as a matter of fact these drops are not formed under ordinary
conditions when water and water vapour alone are present, even though
the vapour is considerably oversaturated, and that for the formation of
rain and fog the presence of dust is necessary. As the water is deposited
around the particles of dust, the drops thus commence with a finite radius,
and so avoid the difficulties connected with their early stages. The effect
of dust on the formation of cloud can be shown very easily by the following
experiment. A and B are two vessels connected with each other by a
flexible pipe ; when B is at the upper level indicated in the diagram the globe
A is partly filled with water ; if the vessel B is lowered the water runs out of
A, the volume of the gas in A increases, and the cooling caused by the
expansion causes the region to be oversaturated with water vapour. If A is
filled with the ordinary dusty air from a room, a cloud is formed in A
whenever B is lowered ; this cloud falls into the water, carrying some dust
with it ; on repeating the process a second time more dust is carried down,
and so by continued expansions the air can be made dust free. We find
that, after we have made a considerable number of expansions, the cloud
ceases to be formed when the expansion takes place ; that the absence of
the cloud is due to the absence of dust can be proved by admitting a little
dust through the tube ; on making the gas expand again a cloud is at once
formed.
It was supposed for some time that without dust no clouds could be
formed, but it has been shown by C. T. E. Wilson that gaseous ions can
act as nuclei for cloudy condensation if the supersatTiration exceeds a
certain value^ and he has also shown that if perfectly dust-free air has its
volume suddenly increased 1*4 time a dense cloud is produced. Though
dust is not absolutely essential for the formation of clouds, yet the
conditions under which clouds can be foimed without dust are very
exceptional, inasmuch as they require a very considerable degree of super-
saturation.
Movement of Camphor on Water. — If a piece of camphor is
scraped and the shavings allowed to fall on a clear water surface they
dance about with great vigour. This, as Marangoni has shown, is due to
the camphor dissolving in the water, the solution having a smaller surface-
tension than pure water ; thus each little patch of surface round a particle
of camphor is surrounded by a film having a stronger surface-tension than its
own, it will therefore be pulled out and the surface of the water near the
bit of camphor set in motion. For the movements to take place the
surface-tension of the water suiface must be greater than that of the
camphor solution ; if the surface is greasy the surface-tension is less than
that of pure water, and may be so much reduced that it is no longer sufficient
to produce the camphor movements. Lord Rayleigh has measured the
thickness of the thinnest film of oil which will prevent the motion of the
camphor ; the thickness was determined by weighing a drop of oil which
was allowed to spread over a known area. He found that to stop
170
PROPERTIES OF MATTER.
the camphor movements (which involved a reduction of the surface-tension
by about 28 per cent.) ala3-orof oil 2 ju^ithick was required (1 fij^ = 10"' cm.),
and that Avith thinner films the movements were still perceptible. This
thickness is small compared with 12 ^/t tlie thickness found by llUcker
and Reinold for black films, but it must be remembered that the surface
which stops the camphor movements is still far from acting as a surface
of oil ; the surface-tension, though less than that of water, is greater than
that of oil. The manner in which the tension of a contaminated water
surface varies with the amount of contamination has been investigated
by Miss Pockels and also by Lord Ptayleigh {Phil. Mag., 48, p. 321). Miss
Pockels determined the surface-tension by measuring the force required to
detach a disc of known area from the surface ; Lord Rayleigh used
Wilhelmy's method. The amount of contamination was varied by confining
the greased surface between strips of glass or metal dipping into the water;
by pulling these apart the area of the greased surface was increased and
therefore the thickness of it diminished, while by pushing them together
the thickness could be increased.
The way in which the surface-tension is aflTected by the thickness of the
layer of grease is shown by the curve (Fig. 137) given by Lord Rayleigh.
d
o
a>
H
O
ca
XJl
/^
Thickness of Oil Film
Fia. 137,
In this curve the ordinates are the values of the surface-tension, the abscissae
the thicknesses of the oil film ; both of these are on an arbitrary scale. It
will be seen that no change in the surface-tension occurs until the thickness
of the oil film exceeds a certain value (about l/x.yu); at this stage the surface-
tension begins to fall rapidly and continues to do so until it reaches the
thickness corresponding to the point C (about 2.i.i.f^.) ; this is called the can^-
plior ])oint, being the thickness required to stop the movemt nts of the cam-
phor particles. After passing this point the variation of the surfac-tension
with the thickness of the film becomes much less rapid. Loril llayleigh
gives reasons for thinking that the thickness lyu./t is equal to the diameter
of a molecule of oil!
CAPILLARITY,
171
Thus, when the amount of contamination is betweeti the limits corre-
sponding to a thickness of the surluce layer bclwcLii 1 fi.fx and the .sinullest
thickness requumTtd gTve the surface-tension ot oil, any diminution in the
contammation such as would be produced by an extension ot tlio surtace
would result inan increase in the surface-tension. This is a principle of
greatlmportance ; it seems first to have been clearly stated by Marangoni.
Suppose we push a strip of metal along a surface in this condition, the metal
will heap up the grease in front and scrape the surface behind, thus the
surface-tension behind the strip will be greater than that in fi'ont, so that
the strip will be pulled back; there will thus be a force resisting the motion
of the strip due to the variation of the surface-tension. This is Marangoni's
explanation of the phenomenon of superficial viscosity discovered by Plateau.
Plateau found that ii i vibrating body such as a compass-needle was
disturbed from its position of equilibiium and then allowed to return to it
(1) with its surface buried beneath the surface of the liquid, (2) with
Fro. 138.
its face on the surface of the liquid, then with certain liquids, of which
water was one, the time taken in the second case is considerably greater
than that in the first. We see that it must be so if the surface of the
liquid is contaminated by a foreign substance which lowers its surface-
tension.
Calming" of Waves by Oil. — Similar considerations will explain the
action of oil in stilHng troubled waters. Let us suppose that the wind
acts on a portion of a contaminated sui'face, blowing it forward ; the
motion of the surface film will make the liquid behind the patch cleaner
and therefore increase its surface-tension, while it will heap up the oil in
front and so diminish the surface-tension ; thus the pull back will be
greater than the pull forward, and the motion of the surface will be i
retarded in a way that could not occur if it were perfectly clean. The
oiled surface acts so as to check any relative motion of the various parts '
of the surface layer and so prevents any heaping up of the water. It is
these heaps of water which, under the action of the wind, develop into a
high sea ; the oil acts not so much by smoothing them down after they
have grown as by stifling them at their birth.
A contaminated surface has a power of self-adjustment by which the
surface-tension can adjust itself within fairly wide limits; a film of such a
liquid can thus, as Lord Rayleigh jsoints out, adjust itself so as to be in
equilibrium under circumstances when a film of a pure liquid would have
to break. Thus, to take the case of a vertical film, if the surface-tension
were absolutely constant, as it is in the case of a pure liquid when the film
172 PROPERTIES OF MATTER.
is not too thin, this film would break, since there would be nothing to
balance the weight of the film. If, however, the film were dirty, a very
slight adjustment of the amount of dirt at diflerent parts of the surface
would be suflicient to produce a distribution of surface-tension which would
ensure equilibrium. It is probably on this account that films to be durable
have_tojiajiiode of a mixture_of substances,~such as soap and water.
Collision of Drops. — If a ]et~of water be turned nearly verticjilly
upwards the drops into which it breaks will collide with each other; if the
water is clean the drops will rebound from each other after a collision, but
if a little soap or oil is added to the water, or if an electrified rod is held
near the jet, the drops when they strike will coalesce instead of
rebounding, and in consequence will grow to a much larger size. This can
be made very evident by allowing the drops to fall on a metal plate ; the
change in the tone of the sound caused by the drops striking against the
plate when an electrified rod is held near the jet is very remarkable.
The same thing can be shown with two colliding streams. If two
streams of pure water stiike against each other in dust-free air, as in
Fig. 138, they will rebound; if an electritied rod is held neai-, however,
they coalesce.
CHAPTER XV.
LAPLACE'S THEORY OF CAPILLARITY.
Contents, — Intrinsic Pressure in a Fluid — "Work required to move a Particle from
the Inside to the Outside of a Liquid— Work required to produce a new Licjuid
Surface— Effect of Curvature of surface— Thickness at which Surface-tension
changes effect of abruptness of transition between two Liquids in contact.
Laplace's investigations on surface-tension throw so much light on this
subject, as well as on the constitution of liquids and gases, that no account
of the phenomena associated with surface-tension would be complete without
an attempt to give a sketch of his theory. Laplace started with the assump-
tion that the forces between two molecules of a liquid, although very intense
when the distance between the molecules is very small, diminish so rapidly
when this distance increases that they may be taken as vanishing when the
distance between the molecules exceeds a certain value c : c is called the
range of molecular action. We shall find that we can obtain an explana-
^^ ..„
1
B ^
^__^ i .
A
Fio. 189.
tion of many surface-tension phenomena even although we do not know
the law of force between the molecules. Let the attraction of an infinite
flat plate of the fluid bounded by a plane surface on a mass m at a point
at a distance z above the surface be ma-^iz)^ where o- is the density of the
fluid ; in accordance with our hypothesis i\/{z) vanishes when z is greater
than c. It is evident, too, that ina-^(z) will be the attraction at a point ou
the axis of any disc with a flat face whose thickness ,is greater than c and
whose diameter is greater than 2c. • •/,'■-.• t_ -
Suppose we imagine a fluid divided into two portions A and 5 by a
plane ; let us find the pull exerted on Bhy A. Divide B up into thin layers
whose thickness is dz ; then if z is the height of one of these layers above the
surface of separation the force on unit area of the layer is equal to a\l/{z)adz ;
CO
hence the pull of ^ on 6 per unit area is equal to cr I \p[z)dz,
0
c
which, since \^{z) vanishes when 2>c,is the same as (T / ■^{z)dz.
0
This pull between the portions A and B is supposed to be balanced by a
pressure called the "intrinsic pressure," which we shall denote by K. K then
CO
is equal to or I ^{z)dz
174 PROPERTIES OF MATTER
We shall find that the phenomena of capillarity require us to suppose
that, in the case of water, the intrinsic pressure is very larg^e. amounting
on the lowest estimate to several thousand atmospheres. We may remark
in passing that the intrinsic pressure plays a very important part in
Van der Waals' Theory of the Continuity of the Liquid and Gaseous States ;
it is the term ajv- which occurs in his well-known equation
[p + 1')(^ - ^') = RT {see p. 129)
We see, too, at once from the preceding investigation that K is equal
to the tensile strength of the liquid, so that if the common supposition
that liquids are as " weak as water," and can only bear very small tensile
stresses without ruptvire, were true, Laplace's theory, which, as we have
seen, requires liquids to possess great tensile strength, would break down
at the outset. We have seen, however, p. 122, that the rupture of
liquids under ordinary conditions gives no evidence as to the real tensile
strength of the liquids, for it was shown that when water and other
liquids are carefully deprived of gas bubbles — in fact, when they are
not broken before the tension~is applied — they can stand a tension of a
great many atmospheres without rupture ; thus on this point the properties
of liquids are in accordance with Laplace's theory.
There is another interpretation of K given by Dupre which enables
us to form an estimate of its value. Consider a film of thickness A
(where A is small compared with c) at the top of the liquid ; the work
required to pull unit of area of this film oft' the liquid and remove it
out of the sphere of its attraction is evidently
or KA
0
Thus the work required to remove unit volume of the liquid and
scatter it through space in the form of thin plates whose thickness is
small compared with the range of molecular atti-action is K. Now the
work required to take one of these films and still further disintegrate
it until each molecule is out of the sphere of action of the others will
be small compared with the work required to tear the film ofl;' the surface
of the liquid ; hence K is the work required to disintegrate unit volumes
of the Kquid until its molecules are so far apart that they no longer
exert any attraction on each other ; in other words, it is the work required
to vaporise unit volume of the gas. In the case of water at atmospheric
temperature this is about GOO thermal units or 600 x 4:-2 x 10' = 25'2 x 10*
mechanical units ; or since an atmosphere expressed in these units is 10®
this would make K equal to about 2."). 000 atmospheres.*
Work required to move a Particle from the Inside to the
Outside of a Fluid. — Consider the force on a particle P at a depth z
below the surface ; the force due to the stratum of fluid above P will bo
balanced by the attraction of the stratum of thickness z below P ; thus
the force acting on P will be that due to a slab of liquid on a particle at
* Van der Waals gives the following value of K deduced from his equation:
water 10,500-10,700, ether 1300-1430 alcohol 2100-2400, carbon bisulphide 2900-2890
atmospheres.
-/
^;^ ' LAPLACE'S THEORY OF CAPILLARITY. 175
a distance z above its surface— i.e., ma^{z). Hence the work done in
bringing the particle to the surface is
00 V
m I a^{z)dz = m(K/o-) ;
as an equal amount of work will be required to take the particle from the
surface out of the range of molecular attraction, the total amount of work
required is thus 2?rt(K/(7).
ITence, ijHi^rticlejxiovingjwith a velocity v towardsthe^urface starts
from a depth greater than c it cannot cross the surface unliss
■kmv > ■ or v > — •
L o- 2
In the case of water, for which a = \ and K on the preceding estimate
is 25,000 atmospheres or 2-5 x 10"-, we see that a particJe^waiilxLxiQt_eross
the surface unless its velocity w^ere greater than 3-2 x 10^. The average
velocity of a molecule of water vapour at 0° C. is about G x lO*, so that if
the water contained molecules of water vapour it would only be those
possessing a velocity considerably greater than the mean velocity, which
would be able to escape across the surface.
Work required to produce a new Liquid Surface. —Let us con-
sider the amount of work required to separate the two portions A and B
into which a plane G divides the liquid. Dividing B up, as before, into
slices parallel to the interface, then the work done in removing the slice,
whose thickness is dz and whose height above the plan© is », is per unit
of area equal to -^^^ ^- ,
00 00 fl ,1 1
er'dz I xp^xjdx = a'dzv^ii V = j \l/{x)dx ILi.,.AJ^
hence the work required to remove the whole of the liquid B standing on '•v^
unit area away from -4 is / a^vdz ;
0
integrating this by parts we see that it is equal to
Ai>
w £«-(-£-%.
J'"-
crzv - I (TZ-^dz
dv
.^iM^ ^•''N'ow the term within brackets vanishes at both limits, and --= - ^{z),
hence the work required is
For this amount of work we have got 2 units of area of new surface,
hence the energy corresponding to each unit of area {i.e., the surface-
tension), which we shall denote by T is given by the equation
Iz ^l)
176
PROPERTIES OF MATTER.
Young, at the beginning of the century, showed how from T and K it
was possible to calculate the range of molecular forces. He did this by
assuming a particular value for the force, but his argument is appliciible
even when we leave the force undetermined.
If \p{z) is always positive, then, since c is the greatest value of z for
which \p{z) has a finite value, we see from equation (1) that
0C5
\iT-c I \p{z)dz
:icK
hence
c>
2T
K
For water T = 75, and if we take K = 25,000 atmospheres = 25 x 10'", then
the above relation shows that c>(]xlO"^ In this way we can get an
FiQ. 140.
inferior limit to the range of molecular action. This method, which was
given by Young, was the first attempt to estimate this quantity, and it
s-eems to have been quite overlooked until attention was recently called to
it by Lord Rayleigh.
It is instructive to consider another way of finding the expression for
the surface-tension. Consider a pomFP inside a liquid sphere (Fig. 140)T
Then, if /-* is at depth d, below the surface, greater than c, the forces acting
on it, due to the attraction of the surrounding molecules, are in
equilibrium ; if the distance of P below the surface is less than c, then
to find the force on F describe a sphere with radius c and centre F, and
LAPLACE'S THEORY OF CAPILLARITY.
177
the force on P, acting towards the centre of the larger sphere, will be
equal to the attraction which would be exerted on P by a quantity of the
fluid placed so as to fill BA CD, the portion of the sphere whose centre is
P, which is outside the larger sphere. This portion may be regarded aa
consisting of two parts — (1) the portion above the tangent plane at A, the
point on the lai'ge sphere nearest to /*, and (2) the lenticular portion
between this plane and the
sphere. Now the attraction A
of the portion above the
tangent plane is the same as
that of a slab of the liquid
extending to infinity and
having the tangent plane for
its lower face, for the por-
tions of liquid which have
to be added to the volume
ADEF to make up this slab
are at a greater distance Fig. 141.
from P than c, and so do
not exert any attraction on matter at P. Thus, if AP = z, the attraction
of AFDE on unit mass at P, using the previous notation, is a-^{z) ; the
attraction of the lenticular portion at P can be shown to be— ;/'(^) where
E is the radius of the liquid sphere. Hence the total force at P acting
on unit mass in the direction AP \^ equal to
'^^(^) + g'^(^)
(3)
Consider now the equilibrium of a thin cylinder of the fluid, the axis of
the cylinder being PA ; divide this cylinder up into thin discs, then if dz
is the thickness of a disc, z its distance from A and a the area of the cross-
section of the cylinder, the force acting on this disc is equal to
|<rV(.)-.^^(.)|a(^«
This force has to be balanced by the excess of pressure on the lower face
of the disc over that on the upper face ; this excess of pressure is, if p
represents the pressure, equal to a—dz;
dz
hence, equating this to the force acting on the disc, we get
f^=^^M^)+a--^-^{z)
Thus the excesa_of pressure at a point at a distance c, below A over the
pressure at^ is equal to
/ cr^^{z)dz + / (r~\l>{z)dz
2T
or with our previous notation K + ^ .
178
PROPERTIES OF MATTER
The pressure has the same value at all points whose depth below the
surface is greater than c. The term 2T/R represents the excess of
pressure due to the curvatui'e of the surface ; we obtained the same value
by a difTerent process on
p. 145. If the surface of
the liquid sphere had been
concave instead of convex,
an inspection of the figure
shows that to obtain the
force on P we should
have to subtract the attrac-
tion due to the lenticular
portion from the attrac-
tion due to the portion
ADE instead of adding
it ; this would make the
pressure at a point in the
mass of the fluid less than
that at a point in the
fluid but close to the
surface by 2T/R.
Thickness at which
the Surface - tension
Chang'eS. — We can determine the point at which the surface-tension
begins to change by finding the change of pressure which takes place as
we cross a thin film. Let Fig. 143 represent the section of such a film,
bounded by spheres ; if the thickness of the film is small, the radii of these
spheres may be taken as approximately equal. Let P be a point in the film,
ABP a line at right angles to both surfaces, then the investigation just
given shows that if AP = z, BP = z', the force on unit mass at P is equal to
when R is the radius of one of the films. We see, too, from the last paragraph
that the pressure at B must be greater than that at A by
t t t
f{amz) + qm]dz - J WW) - i^w)W = ~fzuz)dz
¥lG. 142.
where t is equal to A B, the thickness of the film. Hence, from the for-
mula (p. 145) for the difference of pressure inside and outside a soap
bubble, we may regard
^^
-2 J ^W)dz
as the_^urface-tension of a film of thickness t. Since yl{z^ vanishes when
g_is greater than c, the suija^e-tension_win_reach a constant_value when t
Is as great as c ; hence c. the rangeofmolccular action. ITtLe thickness "of a
LAPLACE'S THEORY OF CAPILLARITY. 179
film when the surface-tension begins to fall off. When t is less than c we
eee from the preceding expression that, T being the surface-tension,
4
J Now if T is represented by a curve like Fig. 134, cTVldt is zero down to P,
y^ positive from P to R, negative from R to T, and positive again for all
^> thinner films; hence, since the force of a slab is attractive when ^ is
positive, repulsive when ;// is negative, this would imply, on Laplace's
theory, that the molecular forces due to a slab of lifxiud at a point outside
_ y^ , Q^re atjirst attrdctioii&4. then, as the p oint gets near ei^ie slab, tliey change
C to repulsions, and change again "
to attractions as the point ap-
pi-oaches still nearer to the slab.
If t is so small that ^^{t) can be
regarded as constant, we see
jjL^f^ZcX^ that T will vary as {-, so that
ultimately the surface - tension
will diminish very rapidly as the
film gets thinner.
On the Effect of the Ab-
ruptness of Transition be- fig. 143
tween two Liquids on the
Surface-tension of their Interface. — Laplace assumed that the range I
of molecular forces was the same for all bodies, and that at equal distances
the force was proportional to the density of the substance. This implies
that the function \p{z) is the same for all bodies. This hypothesis is
certainly not general enough to cover all the facts; it is probably,',
however, sufficiently general to give the broad outlines of capillary
phenomena. Let us calculate on this hypothesis the surface-tension
between two fluids A and 13. Let o-j cr^ be the densities of these fluids;
then to separate a sphere whose area is S from the liquid A requires the
expenditure of work equal to
|S
00
cr,^ / z\p{z)dz {see p. 175)
Let us make a spherical hole of equal size in B. To do this will require
the expenditure of an amount of work equal to
iSff// z-^{z)dz
Let us place the sphere A in the hole in B, and let the fluids come into
contact imder their molecular forces ; during this process the amount of
woi'k done by these forces is
09
\
180 PROPERTIES OF MATTER.
Hence the total expenditure of work required to produce an area S of
interface of A and B is
CO OO 00
iS,7,- fz^|.{z)dz + ^S<t/ fz-^{z)dz - 8a,(T, jzi{z)dz
0 0 0
OO
^m^,-a,yjz-^{z)dz
o
But tins work is by definition equal to T^uS where T^n is the surface-
tension between A and B ; hence we see that T^b = (^x - o-^)"^* where
CO
C = ^ fz^z)dz
is a constant for all substances. This result is not a complete representa-
tion of the surface-tension, for if it were there would always be surface-
tension between liquids of different densities, so that two such liquids
could not mix ; it would also require that the surface-tension between
fluids of equal density should be zero, and that
V Tab = V Tac + v T(
CB
where Tab, Tao and Tcb are respectively the surface -tensions between fluids
A and B, A and C, and B and C respectively. None of these results are in
accordance with experiment. Let us, however, on the assumption that the
surface-tension is represented by an expression of this kind, calculate
(following Lord RayJeigh) the effect of making the transition between
A and B more gradual ; we can do this by supposing that we have between
A and B a layer of a third fluid C whose density is the arithmetical mean
between the densities of A and E; then Tac = i 'i\B = TcB- Hence, though
now wc have two surfaces of sepai'ation instead of one, the energy per unit
area of each is only one quarter of that of unit area of the original suiface ;
hence the total energy due to surface-tension is only one half of the
energy when the traiisition was more abrupt. By making the transition
Betwesfi A and B still Uiore'^ gradual by interposing « liquids whose
densities are in arithmetical progress, we reduce the energy due to surface-
tension to y(n+ 1) of its original value. Thus we conclude that any dimi-
nution in tlie abruptness will diminish the energy due to surface tension.
This result may have important bearings on the nature of chemical action
between the surface layers of liquids in contact, for if a layer of a chemical
compound of A and B were interposed between A and B the transition
between A and B Avould be less abrupt than if they were directly in contact,
and therefore the potential energy, as far as it results from surface-tension,
would be less. Chemical combination between A and B would result in a
diminution of this potential energy. Now anything that tends to increase
the diminution in potential energy resulting from the chemical combina-
tion promotes the combination; the forces that give rise to surface-
tension would, therefore, tend to promote the chemical combination. Thus,
in the chemical combination between thin layers of liquid there is a factor
present which is absent or insignificant in the case of liquids in bulk, and
LAPLACE'S THEORY OF CAPILLARITY. 181
we may expect that chemical combination between thin layers of liquids
might take place even though it were absent in ordinary cases,
Similar considerations would lead us to expect changes in the strength of a
solution near the surface whenever the surface-tension of the solution depends
upon its strength : if the surface-tension increased with the strength there
would be a tendency for the salt to leave the surface layers, while if the
surface-tension diminished as the strength of the solution increased the
salt would tend to get to the surface, so that the surface layers would be
stronger solutions than the bulk of the liquid. The concentration or
dilution of the surface layers would go on until the gradient of the
osmotic pressures resulting from the variation in the strengtlis of different
layers is so great that the tendency to make the pressure equal just
balances the efiects due to surface-teiision.
CHAPTER XVI.
DIFFUSION OF LIQUIDS.
Contents. — Gen6l-al Law of Diffusion — Methods of determining^ the Co-efficictit of
Diffusion — Difl'iision through Membranes. Osmosis — Osmotic Pressure^ Vapour
Pressure of a (Solution — Elevation of the Boilirg-jioint of Solutions — Depression
of the Freezing-point— Dissociation of Electrolytes.
If two liquids are left in contact with each other and are free from the
action of external forces, then if they can mix in any proportion they will
of themselves go on mixing until the whole mass is uniform in composi-
tion. This process may be illustrated by taking a vertical glass tube and
filling the lower part with a strong solution of a coloured salt, such as
copper sulphate. On the top of this clear water is poured very slowly
and carefully, so as not to give rise to any currents in the liquid. The
coloured part will at first be separated from the clear by a shai"ply marked
surface, but if the vessel is left to itself it will be found that the upper
part will become coloured, the colour getting fainter towards the top,
while the colour in the lower part of the
tube will become fainter than it was origin-
ally. This change in colour will go on until
ultimately the whole of the tube is of a
uniform colour. There is thus a gradual
transference of the salt from the ^places
Avhere the solution is strong to those where
it is weak and of water in the opposite
directiqUj^and eqixilibrium is not attained
untiljthe^strength of the solution is uniform.
This process is called difl'usion. In liquids
it is an exceedingly slow process. Thus, if
the tube containing the copper sulphate
solution were a metre long and the lower
half were filled with the solution, the upper
half with pure Avater, it would take con-
siderably more than ten years before the
mixture became approximately uniform ; if the height of the tube were a
centimetre, it would take about ten hours, th^_time required being
proportional to the square of the lengtli^f the tube.
The first~systcmatic experTmeiffcs on diffusion were made by Graham in
1851. The method he used was to take a wide-necked bottle, such as is
Bhown in Fig. 144, and fill it to within a short distance of the top with
the salt solution to be examined; the bottle was then carefully filled up'
with pure water pi-essed from a sponge on to a disc of cork floating on the
top of the solution ; the bottle was placed in a larger vessel filled with
pure water to about an inch above the top of the bottle. This was left
undistui'bed for several days, and then the amount of salt which had
escaped from the battle into the outer vessel was determined. Graham
was in this way able to show that solutions^of the same stx'cugth of
»
Fio. Ut.
DIFFUSION OF LIQUIDS.
183
di5erent_substajicesj[iflus^^ diQerent velocities ; that solutions of_tIie j.'i^Jt
same salt of dUerent stre^tE£_dittuse'a"wItLveIocities proportionalto the 3. l.*tf
8tj;engthX~thatjthe~rate ofdiffusion increased with the temperatureTand -^ ■ /vt
that the^-oportion^ftvvo salts iji admixture was altered by diffusionj and *^ (o^J
that in some cases a decomposition or separation of the constituents of
complicated salts, such as bisulphate of potash and potash alum, could bo
brought about by diflfusion. Though Graham's experiments proved many
important and interesting properties of diffusion, they did not lead to
sufficiently definite laws to enable us to calculate the state of a mixture at
any future time from its state at the present time. This step was made
by Fick, who, guided by Fourier's law of the conduction of heat — the
diffusion of temperature — enunciated in 1855 the law of difl'usion, which
3 4
Ce)'cU.inet3'es
Fig. 145.
6 T r' 1
has been abundantly verified by subsequent experiments. Fick^sjaw may
be stated as follows : Imagine a mixture of salt and water arranged so that
layers of equal density are horizontal. Let the state of the^mixture
be such that^n the layer at^_a height ^^^jibiaveA^ fixed plane there are
n grammes of salt per cubic centimetre; then^ ajsross unit area of^Jjiis
plane R— - grammes of salt will pass in unit time from the side on which i
the soluFion is strongerjtojthat_on which it is weaker. R is^called the
SlfiusiyityjofjEHe^subSaiice ; it depends on the nature of the salt and the
solvent, on the temperature, and to a slight extent on the strength of
the solution! This law is analogous to Fourier's law of the conduction of
heat, and the same mathematical methods which give the solution of the
thermal problems can be applied to determine the distribution of salt
through the liquid. The curves in Figs. 145 and 146 represent the solution
of two impoi'tant problems. The first represents the diffusion of salt from
a saturated solution into a vertical column of water, the surface of separa-
tion being initially the plane x = o. The ordinates represent the amount
of salt in the solution at a distance from the original surface of separation
represented by the abscissse. The times which have elapsed since the
commencement of diffusion are proportional to the squares of the numbers
184
PROPERTIES OF MATTER.
on the gurve ; thus^ if the first curve represents the state of things after
time T, the second represente it after a time 2-^, the third after a time
o-'T, and so on ; for the same ordinate the abscissa on curve 2 is twice
that on curve 1, on curve 3 three times that on curve 1, and so on; thus
the_time required for diffusion through a given length is proportional to
the square of the ^ ^^'
Collected Papers, vol.
T = 25,700 seconds, for
chlorK
length
The curves are copied from Lord Kelvin's
111. p. 432 : for copper sulphate, through water
e througli water
sugar
through
w'ater T= 17,100, and for soclium
T = 5390. The second figure. Fig. 146, represents
the difl'usion when we have initially a thin layer of ealt solution at the bottom
of a vertical vessel, the rest of the vessel being filled with pure water ; the
ordinates represent the amount of salt at a distance from the bottom of
the vessel represented by the abscissae. The times which have elapsed
since the commencement are
proportional to the squares of
the numbers on the curves.
By stirring up a solution
of a salt Avith pure water we
bring thin layers of the solvent
and of the salt near together ;
as the time required for diffus-
ing through a given distance
varies as the square of the
distance, the time required \
for the salt and water to
become a uniform mixture is
greatly diminished by drawing
out the licjuid into these thin (
layers by stirring, and as f
much diftusion will take mueE M^<"^^
in a fe^w^econds as would )
1 IG. ii6.
take place in asmany hours
withoujfc^thejnixing. We can see in a general way why the time required
will be proportioiial to the square of the thickness of the layers ; for if we
halve the thickness of the layers we not only halve the distance the salt
has to travel but we double the gradient of the strength of the solution,
and thus by Fick's law double the speed of diffusion ; thus, as we halve
the distance and double the speed, the time required is reduced to one
quarter of its original value.
Methods of Determining; the Coefficient of Diffusion.— If we
know the original distribution of the salt through the water and the value of
li, we can, by Fourier's mathematical methods, calculate the distribution of
salt after any interval T ; conversely, if we know the distribution after this
interval, we can use the Fourier result to determine the value of R.
Thus, if we have any means of measuring the amount of salt in the
different parts of the solution at successive intervals, we can deduce the
value of R. It is not advisable to withdraw a sample from the solution
and then determine its composition, as the withdi-awal of the .'^ample
might produce currents in the liquids whose effects might far outweigli any
due to pure diffusion ; it is, therefore, necessary; to sample the composition
of the solution when vi situ, and this has been done by measuring some
physical property of the solution yhich^-aries in_aJkiiown way with the
DIFFUSION OF LIQUIDS.
185
strength of the solution. In Lord Kelvin's method the specific gravity is
the pi-operty investigated : theTower halFoTaTvertical vessel is filled with
a solution, the upper half with pure water . C lass beads of difl'erent densities
are placed in the solution ; at first they float at the junction of the solution
and the water, but as diflfusion goes on they separate out, the heavier one?
sink and the lighter ones rise. By noting the position of the beads ol
known density we can get the distribution of salt in the solution, and
thence deduce the value of R. The objection to the method is that air
bubbles are apt to form on the beads when salt will crystallise out on them,
and thus alter their buoyancy. In the case of sugar solutions the strength
ot the diHerent layers can be determined by the rotation of the £lane of
polarisation^ H. F. Weber verified Fick's law in the case of zinc sulphate
solution b^jneasuring the electromotivejforce^ietween two^malgamated
jr^ ~^
\ /
If //
Fio, 147.
zinc^plateg,; he had previously determined how the electromotive force
depends on the strength of the solutions in contact with the plates. The
diffusion^of differen^salts was compared byj^ong ( Wied. Ann. 9, p. Gl 3) by the
metliod shown in Fig. 147. A stream of pure water flows through the bent
tube, a wide tube fastened on to the bent tube establishes commvinication with
the solution in the beaker ; after the water has flowed through the bent tubts
for some time the amount of salt it carries over in a given time becomes
constant. As the water in the tube is continually being renewed, while the
strength of the solution inthe beaker may be regarded as constant, since in
the experiments only a very small fraction of the salt is carried over, the
gradient of concentration in the ueck will be proportional to the strength of
the solution; so that the amount of salt carried ofl' by the stream of water
in unit ~time is proportionaj^o the product of the diffuslvi:ty:_aml,J/he
.strength of the .solutionr By measuring the amount of salt carried over by
the stream in unit time the diffusivities of difl'erent salts can be compared.
As a re.-ult of these experiments it has been found that as a general rule
the_Jn^herjUie_el^cUjc^^ oL a^ solution of a ^alt Jhe more
i^pidly does the salt diffuse. The relative values of the diffusivity for some
of the commoneF salts and acids are given in the table on p. 18G. The
solutions contain the same number of gramme equivalents per litre, and
the numbers in the table aie proportional to the number of molecules of
the salt which cross unit surface in unit time under the same gradient of
strength of solution.
186
PROPERTIES OF MATTER.
cjiibstance.
Substance.
KCl
803
KI
NH^Cl
G89
Nal
:NaCl .
GOO
NH^NO,
LiCl
541
KNO3 .
KCy
707
JSTaNOj .
BaCl,
450
LiNOj .
SnCi;
432
BaN,Oc .
CaCl,
429
SrNA •
MsCl, .
392
(NHJ^SC),
COCl,
300
Na.,SO, .
NiCl,
304
MgSO, .
KBr
811
ZnSO, .
NH^Br
029
CuSO, .
NaBr
509
MnSO, .
'T?«(:a-t-«'t
Va 1 u p s
^l-y.ffas
.,U
f (5ai«e lYo. ^"1-
H.'jjl/ts ^v
These niimbei
s show
that
as a general rule the salts w
bich diffus
\^ ,
823
072
680
007
524
512
050
552
724
078
348
332
316
298
the most
rapidly are those whose solutions have the highest electrical conductivity.
The absolute values of the diffusivity for a large number of substances have
been determined by Schuhmeister {Wien. Akacl. 79, p. 003) and Scheffer
{Chem. Ber. xv. p. 788, xvi. p. 1903). The largest value of the diffusivity
found by Scheffer was for nitric acid ; the diffusivity varied with the
concentration and with the temperature; for very dilute solutions at
90° 0. it was 2 x 10j^^_{cm.)7sec. — i.e., if the strength of solution varied by
one per c«nt. in 1 cm. the amount of acid crossing unit area in one second
would be about one five-millionths of the acid in 1 c.c. of the solution.
For solutions of NaCl the diffusivity was only about one half of this value.
Graham found that the velocity of diffusion of ISTaCl through gelatine was
about the same as through water.
Diffusion throug^h Membranes. Osmosis.— Graham was led by
his experiments on diffusion to divide substances into two cla.sses — crystal-
loid and colloid. The crystalloids, which include mineral acids andTalts,
and^which as a rule canbe~obtame<L in defimte^crystallihe forms, ^fluse
much moi'e>apidtythan the substances called by Graham collo^ds^udLAS
are amorphous and^ow no signs
starch, glass, which
|0
If
the gumsTaTbumen, _^_ ^
of crystallisation^ The^x-ystalloids when dissolved m water change in a
marked degree its properties : for example, they dimihisli tlie vapour
pressure, lower the freezing- and raise the boiling-point. Colloidal sub-
staiices,jwJaen_^issolye4jiIJva^^ any effects^pf this kind,
in fact, many^coIIoHlarsolutions seem~tobeirtHe more than mechanical
mixtures, the colloid in a very finely divided state being suspended in the
fluid. The properties of solutions of this class are very interesting ; the
particles move in the electric field, in some cases as if they were positively,
in others as if they were negatively, charged. The addition of a trace of
acid or alkali is often sufficient to produce precipitation. The reader will
find an account of the properties of these solutions in papers by Picton
and Linder {Journal of Chemical Society, vol. 70, p. 508, 1897 ; vol. 01,
p. 148, 1892); Stoeckl and Vanino {Zeitschrift f. Phys. Chem., vol. 30,
p. 98, 1899) ; Hardy (Proceedings of Poyal Society, 00, p. 110 ; Journal of
Physiology, 24, p. 288). Colloidal substances when mixed with not too
much water form jellies ; the structure of these jellies is sometimes on a
sufficiently coarse scale to be visible under the microscope (see Hardy,
DIFFUSION OF LIQUIDS.
187
Proceedings Royal Society, 6G, p. 95, 1900), and apparently consists of a
more or less solid framework tlirough which the liquid is dispersed.
Through many of these jellies crystalloids are able to difi'use with a
velocity approaching that through pure water ; the colloids, on the other
hand, are stopped by such jellies. Graham founded on this^ method for the
separation of crystalloids and colloidsj^called dialy.sis. In this method a film of
a colloidal substance, such as parchment paper
(paper treated with sulphuric acid) or a piece of
bladder is fastened round the end of a glass tube,
the lower end of the tube dipping in water which is
frequently changed, and the solution of cryfetalloids
and colloids is put in the tube above the parchment
paper. The crystalloids difluse through into the
water, and the colloids remain behind ; if time be
given and the water into which the crystalloids
■diffuse be kept fresh, the crystalloids can be entirely
separated from the colloids.
The passage of liquids_through films of this
kind_ia_jcallei osmosis. The first example of it
seems to have been observed by the Abbe Nollet,
in 1748, who found that wdien a bladder full of
alcohol was immersed in water, the water entered
the bladder more rapidly than the alcohol escaped,
so that the bladder swelled out and almost burst.
If, on the other hand, a bladder containing water
was placed in alcohol the bladder shrank.
The motion of fluids throvigh these membranes
can be observed with very simple apparatus : all
that is necessary is to attach a piece of parchment-
paper firmly on the end of a glass tube, the upper
portion of which is drawn out into a fine capillary
tube. If this tube is filled with a solution of sugar
and immersed in pure water, the top of the liquid
in the capillary part of the tube moves upwards
with sensible velocity, showing the entrance of
water through the parchment-paper. Graham
regarded this transport of water throughT the
membrane as due to this colloidal substance^being
able to hold more wateFln^ombination when in
contact with pure waterjthan when in^contsct wjtb
ar~salt solution ; thus, when the hydration of the
membrane^orresponding to the side next the water
extends to the side next the solution, the membrane Fio. 148.
cannot hold all the Avater in combination, and some
of it is given up ; in this way water is transported from one side of the
membrane to the other.
Membranes of parchment-paper or bladder are permeable by crysta-lloids
as well jis by wateri There are otTier memBranes, however, whicETwhile
permeable to water are impermeable to a large number of salts ; these
membranes are called semi-permeable membi-anes. One of these, which
has been extensively used, is the^elatinous precipitate of ferrocyanide of
copper, which is produced when copper sulphate and potassium ferro-
E^
188
PROPERTIES OF MATTER.
cyanide come into contact. This jrccipitate is mechanically exceedingly
Weak, but Pfeffer made serviceable membranes by precipitating it in the
pores of a poi-ous pot. If such a pot is filled with a very dilute solution
of copper sulphate and immersed in one of ferrocyanide of potassium the
two solutions will diffuse into the walls of the pot, and where they meet
the gelatinous precipitate of ferrocyanide of copper will be formed ; in this
way a continuous membrane may be obtained. For details as to the pre-
cautions which must be taken in the preparation of these membranes the
reader is referred to a paper by Adie {Froceedings of Chemical Society/,
lix. p. 344). If a membrane of this kind be deposited in a porous pot
fitted with a pressure gauge, as in Fig. 148, and the pot be filled with a
dilute solution of a salt and immersed in pure water, water will flow into
the pot and compress the air in the gauge, the
pi-essure in the pot increasing until a definite
pressure is reached depending on the streugth
of the solution. When this pressure is'
I'eached thei-e is equilibrium, and there is no
further increase in the volume of water in-
the pot.
Osmotic Pressure. — Thus the flow of
water through the membrane into the
stronger solution can be prevented by apply-
ing to the solution a definite pressure ; this
pressure is called the osmotic pressure of the
solution. It is a quantity of fundamental
importance in considering the properties of
the solution, as many of these properties,
such as the diminution in the vapour pres-
sure, and the lowering of the freezing-point,
are determinate as soon as the osmotic
pressure is known.
The work done when a volume v of
water passes across a semi permeable mem-
brane from pure water into a solution where
the osmotic pressure is P is equal to Pv.
For, let the solution be enclosed in a vertical
■Water tube closed at the bottom by a semi-permeable
membrane, then when there is equilibrium
the solution is at such a height in the tube
that the_pressure^^aiLjthe_inembrane due to
the head of the solution is equal to the
osmotic pressure. When the system is m
equilibrium we know by Mechanics tMt the total work done during any
small alteration of the system must be zero. Let this alteration consist in
a volume v of water going through the semipermeable membrane. This
will raise the level of the solution, and the work done against gravity is
the same as if a volume v of the solution were raised from the level of the
membrane to that of the top of the liquid in the tube. Thus the work done
against gravity is vgph, where h is the height of the solution in the tube
and p the density of the solution ; since the pressui^e due to the head of
solution is equal to the osmotic pressure, gph = F. Hence the work done
against gravity by this alteration is Pv, and since the total work done
'-:
■ScUUtfifl
Membrane
Fio 149.
DIFFUSION OF LIQUIDS.
189
must be zero, the work done on the liquid when it crosses the membrane
must be Py.
The values of the osmotic pressures for different solutions was first
determined by Pfefler,* who found the very remarkable result that for
weak solutions Avhich do^ not conduct electricity the osmotic pressure is
equal to the gaseous pressure which would be exerted by the molecules of
the salt if these were jnJ^the'gasebusYtate and occupying a volume equal
to_that of the solvent in which the salt is dissolved. Thus, if 1 gramme
equivalent of the salt were dissolved in a litre of water the osmotic pressure
would be about 2'2 atmospheres, which is the pressure exerted by 2
grammes of hydrogen occupying a litre. Pfeffer's experiments showed
that approximately, at any rate, the osmotic pressure_wa8, like the^pregsure
of a gas, proportional to the absolute temperature. If the cell is placed in
another solution instead of pure water, water will tend to run into the cell
if the osmotic pressure of the solution in the cell is greater than that of
the solution in which it is immersed, while if the osmotic pressure in the
cell is less than that outside the volume of water in the cell will decrease ;
if the osmotic pressure is the same inside and outside there will be no
change in the volume of the water inside the cell. Solutions which have
the same osmotic pressure are called
method
of
pressure are called isotonic solutions. A convenient
finH^ing the strengtEs of solutTons or dillerent salts which are
He showed that the membrane lining
4.
I
isotonic was invented by De Vries
the cell-wall of the leaves of some plants, such as Tradescantia discolor,
Curcuma ruhricaidis, and Begonia manicata, is a semi- permeable membrane,
being permeable to water but not to salts, or at any rate not to many
salts. The contents of the cells contain salts, and so have a definite osmotic
pressure. If tb.ese cells are placed in a solution having a greater osmotic
pressure than their own, water will run fi-om the cells into the solution,
the cells will shrink and will present the appearance shown in Fig. 1 50 b.
Fig. 150 a shows the appearance of the cells when surrounded by water;
the weakest solution which produces a detachment of the cell will be
approximately isotonic with the contents of the cell. In this way a series
* PfefTer, Osmotischc Untcrsuchungcn, Leipzig, 1877.
f De Vries, Zcit. f. Physik. Chemie, ii. p 415
190
PROPERTIES OF MATTER.
WaXer vapour.
of solutions can be prepared which are isotonic with each other. De Vrie»
found that for noi\-electroly tes isotonic solutions contained in each unit of
volume a weight ofjhe salt proportional to the molecular^weight ; in other
wor3s, thatjsptpnic^solutions of non-electrolytes contain the same number
of molecules of the salt. ThisTs^iiother instance of the analogy between
osmotic pressure an^ gaseous pressure, for it is exactly analogous ta
Avogadro's law, that when the gaseous pressures are the same all gasea
at the same tempei'ature contain the same number of molecules per unit
volume. Although the direct measurements on osmotic pressure hitherto
made may seem a somewhat slight base for the establishment of such an
important conception, an immense amount of experimental woik has been
done in the investigation of such phenomena as the lowering of the vapour
pressure, the raising of the boiling- and the lowering of the freezing-point
produced by the solution of salts in water. The conception of osmotic
pressm*e enables us to calculate the magnitude of these effects from the
strength of the solution ;
M^nxhra^ ^j^g agreement between the
values thus calculated and
the values observed is so
\faier '■apour closB ES to furnish strong
evidence of the truth of
this conception.
Vapoup Pressure of
a Solution.— The change
in the vapour pressure due
to the presence of salt in
the solution can be calcu-
lated by the following
method due to Van t'
Hoff: Suppose the salt
solution A, Fig. 151, is
divided from the pure water 5 by a semi-permeable membrane — i.e., one
which is permeable by water and not by the salt ; transfer a small
quantity of water whose volume is v from ^1 to B by moving the
membrane from right to left. If IT is the osmotic pressure of the solu-
tion the work required to effect this transference is Hv ; now let a volume
V of water evaporate from B and pass as vapour through the membrane into
the chamber ^1 and there condense. If Y is the volume of the water vapour,
Ip the excess of the vapour pressure of the water over B above that over A^
the work done in this process is cpY. The process is clearly a reversible one,
and hence by the Second Law of Thermodynamics, since the temperatures
of the two chambers are the same, there can be no loss or gain of mechanical
work. Thus, since the work spent in one part of the cycle must be equal
to that gained in the other, we have
Solution,
WaXcr
' Memhrano
Fia. 151.
Suppose p is the vapour pressure over the water, let V be the volume
occupied at atmospheric pressure IT,, by the quantity of water vapour which
at the pressure p occupies the volume V ; then by Boyle's Law,
n„v'=pV
DIFFUSION OF LIQUIDS.
191
80 that
but for water vapour vfV' = 1/1200, hence
lp_ n 1
p Uo 1200
WfXter vcLpotKr
cuui. atr
SoUxti^n,^
Water vapour
oTUi air
Wojt^r
The osmotic pressure in a solution of 1 gramme equivalent per litre , , c^
of a salt which Joes not dissociate when dissolved is about '22 atmospheres ;
thus for such a solution
8p_ 22
p 12U0
or the vapour pressure over the solution is nearly 2 per cent, less than
over pure wat^ ,^
IftEe surface of the solution is subjected to a pressure equal to
the osmotic pressure the vapour pressure over the^ solution will increase
and^ wilT be equal to the
pressure over pure water.
For let Fig. 152 represent a
vessel divided by a dia-
phragm permeable only by
water and by water vapour,
and let the salt solution in
A be subject to a pressure
equal to the osmotic pres-
sure. Under this pressure
the liquids will be in equi-
librium, and there will be
no flow of water across the diaphragm. If the vapour pressure of the
water is greater than that of the salt solution, then water vapour from B
will go across the diaphragm and will condense on A • this will make
the solution in A weaker and reduce the osmotic pressure. Since the
external pressure on A is now greater than its osmotic pressure, water
will flow from ^ to ^ across the diaphragm ; thus there would be a
continual circulation of water round the system, which would never be
in equiUbrium. As this is inadmissible, we conclude that the vapour
pressure of the water is not greater than that of the solution ; similarly if
it were less we could show that there would be a continual circulation in
the opposite direction ; in this wa}'^ we can show that the vapour pressure
of the solution when exposed to the osmotic pressure is equal to that of
pure water. This is an example of the theorem proved in J. J. Thomson's
Applications of Bi/namics to Physics and Chemistry, p. 171 (see also Poyn-
ting, Phil. Mag. ,'sii. p. 39), that if a pressure of n atmosphei^es be apphed
to the surface of a liquid the vapour pressure of the liquid, p, is increased
by Ip, where
Memhrcuna
Fig. 152.
hp
V
n
density of the vapour at atmospheric pressure
density of the liquid
Raising" of the Boiling-point of Solutions.— The determina-
tion of the vapour pressure is attended with considerable difficulty, and it
192
PROPERTIES OF MATTER.
B
Solution,
Water
is much easier to measure the effect of salt on the boiling- or freezing-point
of the solution.
Let A and B be vessels containing respectively salt solution and pure
water, separated by a semi-permeable membrane, and let the temperatures
of the vessels be such that the vapour pressure over the solution is the
same as that over pure water. Let 0 be the absolute temperature of the
water, d + cd that of the solu-
tion. Now suppose a volume
■y of water flows from B to A
across the diaphragm ; if 11 is
the osmotic pressure of the
solution, mechanical work llu
will be done in this operation.
Let this quantity of water be
evaporated from A and pass
through the walls of the
diaphragm and condense in
B. As the vapour pressui-es
are the same in the two
cases, no mechanical work is
gained or spent in this opera-
tion. The system is now in
its original state, and the operation is evidently a reversible one, so that
we can apply the Second Law of Thermodynamics. Now by that law we
have
Heat taken from the boiler Heat given up in the refrigerator
Absolute temperature of boiler Absolute temperature of refrigerator
Mechanical work done by the engine
Difierence of the temperatures of boiler and refrigerator.
In our case the mechanical work done is Uv. The heat given up in the
refrigerator is the heat given out when a volume v of water condenses
fiom steam at a temperature d; if X is the heat given out when unit mass
of steam condenses and a the density of the liquid, the heat given out in
the refrigerator is "Kav ; hence by the Second Law we have
Fio. 153.
Xo-y TIv
— = — or
9 od
dd
d
n*
x^
Let us apply this to find the change in the boiling-point produced by
dissolving 1 gramme equivalent of a salt in a litre of water ; here II
is 22 atmospheres, or in C.G.S. units 22 x 10^ X is the latent heat of
steam in mechanical units — i.e, 536 x 4-2 x 10', <t is unity, and 0 = 373;
hence
m =
373x22xl0«
53Gx4-2x 10^
= '37 of a degree.
The experiments of Raoult and others on the raising of the boiling-
point of solutions of organic salts which do not dissociate have shown
* The heat given out or taken in by the volume of water when going from one
chamber to the other is negligible in comparison with that required to vaporise the
water
DIFFUSION OF LIQUIDS.
193
(
that the amount of the rise in the boiling-point is almost exactly '37 of
a degree for each gramme equivalent per litre, a result which is strong
confirmation of the truth of the theory of osmotic piessure.
Lowering- of the Freezingrpoint of Solutions.— A similar in-
vestigation enables us to calculate the depression of the freezing-point
due to the addition of salt. Let yl, B (Fig. 15-1) represent two vessels
separated by a semi-permeable membrane, A containing the salt solution
at its freezing-point and B pure water at its freezing-point. Let a volume
V of water pass across the seuii- permeable membrane from B to A ; if 11 is
the osmotic pressure of the solution, mechanical work \lv will be gained by
this process. Let this quantity of water»be frozen in A, the ice produced
taken from A placed in 1>, and there melted. The system has now returned
to its original condition, and the process is plainly reversible ; hence we can
Mertxhrtxnjt
Va/er vof) 0 ur_ ^
SoluXicn,
_ Water vapou^
WcUer
Fig. 154.
apply the Second Law of Thermodynamics. If d is the absolute tempera-
ture of the freezing-point of pure water, 6 - cO that of the freezing-point
of the solution, if X is the latent heat of water, and o- its density ; the
heat taken from the hot chamber B at the temperature 6 is Xcxv ; hence
by the Second Law we have
Thus in the case of water for which 0 = 273, X = 80 x 4-2 x 10^ a=l and
when the strength of the solution is 1 gramme equivalent per litre,
n = 22xl0''; hence 30 = 1-79°.
This has been verified by Raoult in the case of solutions of organic
salts and acids. The result of the comparison of theory with experi-
ment for a variety of solvents is shown in the following table :
Solvent
Acetic acid . .
Formic acid .
Benzene
Nitro-benzene
Ethylene-dibromide
Lowering of freezing point for organic salts,
1 gramme molecule dissolved in a litre
Observed Calculated
3-9
2-8
4-9
7-05
11-7
3
2
5
6
11
'88
•8
•1
■9
•9
N
194 PROPERTIES OF MATTER.
Dissociation of Electrolytes.— The preceding theory gives %
satisfactory account of the efl'ecb upon the boiling- and freezing-points
produced by organic salts and acids when the osmotic pressure is
calculated on the assumption that it is equal to the gaseous pressure
which Avould be produced by the same weight of the salt if it were
gasified and confined in a volume equal to that of the solvent. When,
however, mineral salts or acids are dissolved in water, the eflect on the
boiling- and freezing-points produced by oi gramme equivalents per litre is
greater than that produced by the same number of gramme equivalents of
an organic salt, although if the osmotic pressure were given by the same
rule, the effects on the freezing- and boiling-points ought to be the same
in the two cases. The osmotic pressure then in a solution of a mineral
salt or acid is greater than in one of equivalent strength (i.e., one
for which n is the same) of an organic salt or acid ; this has been
verified by direct measurement of the osmotic pressure by the methods
of Pfefler and De Vries. This increase in the osmotic pressure ia
explained by Arrhenius as being due to a partial dissociation of the
molecules of the salts into their constitutents ; thus some of the
molecules of KaCi are supposed to split up into separate atoms of
Na and 01. Since by this dissociation the number of individual
particles in unit volume is increased, the osmotic pressure, if it follows
the law of gaseous pressure, Avill also be increased. According to
Arrhenius, the atoms of Na and 01 into which the molecule of the salt
is split are charged respectively with positive and negative electricity,
which, as they move under electric forces, will make the solution a
conductor of electricity. In this way he accounts for the fact that
those solutions in which the osmotic pressure is abnormally large are
I conductors of electricity, and that, as a rule, the greater the conduc-
tivity the greater the excess of the osmotic pressure. This view, of
v,'hich an account will be given in the volume on Electricity, has been
very successful in connecting the various properties of solutions.
Though the osmotic pressure plays such an important part in the
theory of solution, there is no generally accepted view of the Avay in Avhich
the salt produces this pressure. One view is that the salt exists in the
interstices between the molecules of the solvent in the state corresponding
to a perfect gas. If the volume of these interstices bore a constant
proportion to the volume of the solvent, then, whatever this ratio may be,
we should get the ordinary relation between the quantity of salt and
the osmotic pressure to which it gives rise. For, suppose p is the
pressure of the gaseous salt, v the volume of the interstices, V the volume
of the solvent ; then if a semi-permeable membrane be pushed so that a
volume hV of water passes through it, and 11 is the osmotic pressure,
then the work done is n5V; but if ^v is the diminution in the volume
I of the interstices, the work done is j)lv ; hence
UhY=pdv
But if the volume occupied by the intei'stices bears a constant ratio to
that of the solvent
V V
where V is the volume of the solvent ; hence
DIFFUSION OF LIQUIDS. 196
nV=;;y or II -^J;
that is, the osmotic pressure is the same as if the gaseous salts occupied
the whole volume of the solvent.
Another view {see Poynting, JPhil. Mag. 42, p. 289) is that the
phenomenon known as osmotic pressure arises from the molecules of salt
clinging to the molecules of the water, and so diminishing the mobility and
therefore the rate of diflusion of the latter. Thus, suppose we have pure
water and a salt solution separated by a semi-permeable membrane, since the
water molecules in the solution are clogged by the salt they will not be able
to pass across the membrane as quickly as those from the pure water, and
there will be a flow of water across the membrane from the pure water
to the solution. Poynting shows that the mobility of the molecules of
a liquid is increased by pressure, so that by applying a proper pressure
to the solution we may make the mobility of the molecules of water in
it the same as those of the pure water, and in this case there will be no
flow across the membrane ; the pressure required is the osmotic pressure.
Poynting shows that this view Avill explain the properties of inorganic
Baits if we suppose that each molecule of salt can completely destroy the
mobility cf one molecule of water.
CHArTER XVII.
DIFFUSION OF GASES.
Contents. — Co-eflicient of Diffusion — Diffusion of Vapours— Explanation of DilTu-
sion on Kinetic Tiieory of Gases — Effects of a Terforatcd Diaphrapra — I'a.-sage of
Gases through Porous Bodies — Thermal Effusion — Atmolvsis — Passage of (Jasea
through Indiarubber, Liquids, Hot Metals — Diff'usion of iletals through Metal.
Ip a mixture of two gases A and B is confined in a vessel the gases
will mix and each will ultimately be uniformly difl'used through tlie vessel
as if the other were not present. If they are not uniformly mixed to
begin with, there will be a flow of the gas A from the places where the
density of A is great to those where it is small. The law of this diflfusion
is analogous to that of the conduction of heat or to the difTusion of liquids
and may be expressed mathematically as follows : Suppose the two gases
are arranged so that the layers of equal density are horizontal planes, and
let p be the density of A at a height x above a fixed horizontal plane ; then
in unit time the mass of A which passes downward through unit area of a
horizontal plane at a height x is proportional to the gradient of p and is
equal to K-^ where K is the interdifFusity of the gases A and B. The
^ dx ^- ■
value of K has been measui^ed by Loschmidt* and Obermayerf for a
considerable number of pairs of gases. The method employed by these
observers was to take a long vertical cylinder separated into two parts by a
disc in the middle. The lower half of the cylinder was filled with the
heavier gas, the upper half with the lighter. The disc was then removed
with great care so as not to set up air cm-rents, and the gases were then
allowed to diffuse into each other ; after the lap^e of a certain time the
disc was replaced and the amount of the heavier gas in the upper half of
the cylinder determined. From this the value of K was determined on
the assumption (which is probably only approximately true) that the
value of K does not change when the pi-oportions of the two gases ai-e
altered. WaitzJ used a diffei-ent method to determine the coefficient of
interdifiusion of air and carbonic acid ; beginning with the carbonic acid
below the air he measured by means of Jamin's interference refractometer
the refractive index of various layers after the lapse of definite intervals of
time ; from the refractive index he could calculate the proportion of air and
carbonic acid gas, and was thus able to follow the course of the diffusion.
iHe found that the coefficient of diffusion depended to some extent on the
jproportion between the two gases, the values of K at atmospheric pressure
fat 0° C. varying between •1288 and 'ISCG cm. -/sec. The values found by
Loschmidt and v. Obermayer are given in the following table. They are
for 76 cm. pressure and 0° C:
• Loschmidt, Wien. Berichte, 61, p. 367, 1870, 62, p. 463, 1870.
J Obermayer, Wien. Berichte, 81, p. 162, 1880.
Wailz, Wiedemann t Annalai, 17, p. 201, 1882.
DIFFUSION OF GASES.
197
Gases.
CO,
-N,0
CO.
-CO.
CO,
-0, .
CO,
- Air
CO,
-CH,
CO,
-H,
CO,
-C,H,
CO-
-0. .
CO-
-H, .
CO
-C.,fT,
so,
-H, .
0,-
H, .
0.-
N, .
0,-
Air .
H,-
■Air .
H,-
■CH,
H,-
■N,0
H.-
-O.H,
LOSCUMIDT.
VON Obkhmaybk.
K cm.7sec.
Kcm.'^sec.
•09831
. •09166
•14055
. -13142
•14095
. -13569
•14231
. -13433
•15856
, -14650
•55585
•53409
•10061
•18022
. -18717
•G4223
•64884
•11639
•48278
•721 G7
•66550
-17875
. -17778
•63405
•62544
•53473
— ,
-45933
— ,
-48627
H,-0,H,
We may, perhaps, gain some idea of the rapidity of diffusion by saying
that the rate of equalisation in composition of a mixture of hydrogen and
air is about half that of the equalisation of temperature in copper.
As an example of the rate at which diffusion goes on we may quote the
result of an experiment by Graham on the diffusion of CO^ into air.
Carbonic acid was poured into a vertical cylinder 57 cm. high until it filled
one- tenth of the cylinder. The upper nine-tenths of the vessel was
filled with air and the gases were left to diffuse. They were found to be
very approximately uniformly distributed throughout the cylinder after
the lapse of about two hours. As the time taken to reach a state of
approximately uniform distribution is proportional to the square of the
length of the cylinder, if the cylinder were only one centimetre long
approximately uniform distribution would be attained after the lapse of
about two seconds.
The intei'diffusity is inversely proportional to the pressure of the
mixed gas ; it increases with the temperature^ According to the' experi-
ments of Losclimidt and v. Obermayer it is proportional to 0" where 0 is
the absolute temperature and n a quantity which for different pairs of
gases varies between 1^75 and 2.
Diffusion of Vapours. — The case when one of the diffusing gases
is the vapour of a liquid is of special importance, as it is on the rate
of diffusion that the rate of evaporation depends. The methods which
have been employed to measure the rate of diffusion of the vapour of a
liquid consist essentially in having some of the liquid at the bottom of a
cylindrical tube and directing a blast of vapour-free gas across the mouth
of the tube. When the blast has been blowing for some time a uniform
gradient of the density of the vapour is established in the tube^ the value
of this is hjl where h is the maximum vapour pressure of the liquid at the
temperature of the experiment and I the distance of the surface of the
liquid from the mouth of the tube. The mass of vapour which in unit
198 PROPERTIES OF MATTER.
time flows out of the tube — {i.e., the amount of the liquid which evaporates
in unit time and which can therefore be easily measured), is K.S/l where K
is the difTusivity of the vapour into the gas; as ^ is known we can readily
determine K by this method. A few of the results of experiments made
by Stefan* and Winkelmannt are given in the following table :
Valuk of K in
cm.7sec. AT
0°C.
AND
760 mm.
Pressube.
Hj-drogen,
Air,
Carbonic acid.
Water- vapour
. •G87
•198
•131
Ether
. -296
•0775
•0552
Carbon-bisulphide
. -309
•0883
•0629
Benzol
. ^294
•0751
•0527
Methyl-alcohol .
. -5001
•1325
•0880
Ethyl-alcohol
. -3800
•0994
•0G93
Explanation of Diffusion on the Kinetic Theory of Gases.—
The kinetic theory according to which a gas consists of a great number of
individual particles called molecules in rapid motion, affords a ready ex-
planation of diffusion. Siipjiose Ave have two layers A and B in a mixture
of gases and that these layers are separated by a plane 0. Let there be
more molecules of some gas y in A than in B, then since the molecules are
in motion they will be continually crossing the plane of separation, some
going from A to B and some from B to A, but inasmuch as the molecules
of 7 in A are more numerous than those in B, more will pass from A to B
than from B to A. Thus, A will lose and B gain some of the gas y ; this
will go on until the quantities of y in unit volumes of the layers A and B
are equal, when as many molecules will pass from A to B as from B to A,
and thus the equality, when once established, will not be disturbed by the
motion of the molecules. It follows from the kinetic theory of gases
(see Boltzmann, Vorlesungen ilher Gastheorie, p. 91) that, if there ai^e n
molecules of y in unit volume of B, n + hi in a unit volume of A at a
distance 2cc from that in B, and if x be measured at right angles to the
plane separating the layers, then the excess of the number of molecules
of y which go across unit area of C from A to B over those which go from
A to B is equal to •3502Xc — , where X is the mean free path of the molecules
dx
of y and c, their average velocity of translation ; the quantity Xc is evidently
proportional to the diffusity.
Now c only depends upon the temperattire, being proportional to the
square root of the absolute temperature, while X is inversely proportional
to the densit}', and if the density is given it does not, at least if the
molecules are regarded as hard elastic spheres, depend upon the tempera-
ture. If the pressure is given, then the density will be inversely, and
X therefore directly pi'oportional to the absolute temperature. Thus, on
this theory the coeliicient of diflusion should vary as ei where 0 is the
absolute temperatute. The experiments of Loschmidt and von Obermayer
seem to show that it varies somewhat more rapidly with the temperature.
Another method of regarding the process of diffusion, which for some
purposes is^f g'reat utility, is as follows : The diffusion of one gas A
through another B when the layers of equal density are at right angles to
* Stefan, Wicn. Alad. Bcr., ef), p. 823, 1872.
t Winkelmann, ]Vkd. Ann., 22, pp. 1 aud 152, 1884.
DIFFUSION OF GASES. 19f)
the axis x may be regarded as due to a current of the gas A moving
parallel to the axis of x with a certain velocity ic through a current of B
streaming with the velocity v in the opposite dii^ection. To move a current
of one gas through another requires the application of a force to one gas in
one direction and an equal force to the other gas in the opposite direction.
This force will be proportional (1) to the relative velocity ti + v of the two
currents, (2) to the number of molecules of A per unit volume, and (3) to
that of the molecules of B. Let it then per unit volume of gas be equal
to Aj3 p^p^ (u + v), where Aj^ is a quantity depending on the nature of the
gases A and B, but not upon their densities nor upon the velocity with which
they are streaming through each other ; pj and p^ are respectively the
densities of the gases A and B — i.e., their masses per unit volume. Hence,
to sustain the motion of the gases a force Ajg p^ p^ (u + v) parallel to x must
act on each unit of volume of A and an equal force in the opposite
direction on each unit volume of B. These forces may arise in two ways;
there may be external forces acting on the gases, and there may also be
forces arising from variations in the partial pressures due to the two
gases. Let Xj, X^ be the external forces per unit mass acting on the gases
A and B respectively, and Pi,p.^ the partial pressui-es of the gases A and B
respectively. Considering the forces acting parallel to x on unit volume
of A, the external force is Xjp,, and the force due to the variation of the
partial pressure is - dp^jdx ; hence the total force is equal to — dpjdx + Xjpj,
and as this is the force driving A through B we have
"Tfi + ^iPi = ^i2Pi/'2(^ + ^) 0)
dx
similarly, _ J^4.X_,p2= - A„p,p,(w + v) (2)
Let us consider the case when there are no external forces and when
the total pressui'e p^ +2^2 ^^ constant throughout the vessel in which
difiusion is taking place. In this case the number of molecules of A
which cross unit ai-ea in unit time must equal the number of molecules of
B which cross the same area in the same time in the opposite direction.
Let this number be q ; then if n^ n^ are respectively the numbei'3 of
molecules of A and B per unit volume,
q = n^u = n^v
If wij, mj are the masses of the molecules of A and B respectively
hence A^^p^p.^ii + v) = A ^^m^m.^n^ + n.^q
Now n^ + n^ is proportional to the total pressure, and aa this is
constant throughout the volume, ?i, + n^ will be constant. Putting X = 0 in
equation (1) and writing N for n^ + n^, we get
1 dp.
9= -
Aypi^m^ dx
Now ^3 = 1^
n.
200 PROPERTIES OF MATTER.
where v„ is the number of molecules of a gas in unit volume at a standard
pressure 2^0 i
hence (7 = - - — ^ -^
Now q is the number of molecules of A pnssinc: unit suiface in unit
time and dvjdx is the gradient of the number per unit volume ; hence,
from the definition of K, the interdifiusity, given on p. lUC, we see
or if P is the total pressure
K= ' /M'
m^n.^K^\no
w 0
Thus, if A, 3 is constant, K varies inversely as P, and directly as {pjn^''.
Since the pressure of a given number of molecules per unit volume is
proportional to the absolute temperature, K, if Aj^ is constant, varies
directly- as the square of the absolute temperature.
We can determine A,2 if we know the velocity acquired by one of the
gases A when acted upon by a known force. Suppose that the gas A is
uniformly distributed, so that dp^jdx = 0, and that when acted upon by a
known force it moves through B with a velocity ?t ; svxppose, too, that B is
very largely in excess and is not acted upon by the force, we have then v
very small compared with u, and from equation (1) we have
A -^
Thup, if we know ?«, the velocity acquired under a known force X, we can
find A,,, and hence K, the diffusivity. This result is of great importance
in the theory of the difiusion of ions in electrolytes, and Nernst haa
developed an electi^olytic theory of diffusion in fluids on this basis.
Another important application of this result is to determine X from
measurements of K and ic. Thus, to take an example, if the particles of
the gas A are charged with electricity and placed in an electric field of
known strength, the force X will depend upon the charge ; hence, if in this
case we measui^e (as has been done by Townsend) the values of K and ic,
we can deduce the value of X, and hence the charge carried by the
particles of A .
On the Obstruction offered to the Diffusion of Gases by a
perforated Diaphrag'm. — if a perforated diaphragm is placed across a
cylinder it does not diminish the difi'usion of gases in the cylinder in the
ratio of the area of the openings in the diaphragm to the whole area of
the diaphragm, but in a much smaller degree, for the eftect of the per-
foration is to make the gradient in the density of the gases in the neigh-
bourhood of the hole greater than it would have been if the diaphragm
had been removed, and therefore the flow through the hole greater than
through an equal area when there is no diaphragm. Thus, to take a case
investigated by Dr. Horace Brown and Mr. Escombe {Proceedings Royal
Society, vol. 07, p. 121), suppose we have OO3 in a cylinder, and place
across the cylinder a disc wet with a solution of caustic alkali which
DIFFUSION OF GASES. 201
absorbs the CO^, so that the density of the COj next the disc is zero.
Then if p is the density of the CO, at the top of the cylinder, the density
gradient is p/l where I is the distance between the disc and the top of the
cylinder, so that the amount of 00^ absorbed by unit area of the disc
it will be^^g/Z^ where k is the diffusivity of CO, through itself. Now suppose,
L." insteadofa disc extending completely across the cylinder, we have a much
smaller disc of radius a, then at the disc the density of the CO^ will be
zero, but it will recover its normal value p at a distance from the disc
proportional to a ; thus the gradient of density in the neighbourhood of
the disc will be of the order p/a and not p/l, and the amount of CO,
absorbed by the disc will be proportional to k (p/a) ttot — i.e.. will be
proportional to a; so that the absorption of the CO, will only diminish as I
the radius of the disc and not as the area. This was verified by Brown
and Escombe, and it has very important applications to the passage of
gases thi-Qugh the openings in the leaves of plants.
Passag'e of Gases through Porous Bodies.— There are ^hr^
^ocesses_by^ jvhicli gas may^jass through a^olid__perforated by a series of
holesor canals ; the size of the holes or pores determining the method by
which the gas escapes. If the plate is thin and the pores are not
exceedingly fine, the gas escapes by what is called effusion ; this is the
process by which water or air escapes from a vessel in which a hole is
bored. The rate of escape is given by Torricelli's theorem, so that the Y^ t ^
velocity with which a gas streams through an aperture into a vacuum is ^
proportional to the square root of the quotient of the pressure of the gas
by its density, and thus for different gases under the same pressure the
velocity will vary inversely as the square root of the density of the gas.
Bunsen foiinded on this result a method of finding the density of gases. oC^
This case, strictly speaking, is not one of diflusion at all, but merely the
flow of the gas as a whole through the apeiLure. If the gas is a mixture
of different gases its composition will i\ot be altered when the gas passes
through an aperture of this kind.
The second method is the one which occurs when the holes are not too
fine, and when the thickness of the plate is large compared with the
diameter of the holes. In this case the laws are the same as when a gas
flows through long tubes; they depend on^the viscosity of the gas, and are
discussed in the chapter relating to that property of bodies. No change
in the composition of a mixture of gases is produced when the gases are
forced through apertures of this kind ; this is again a motion of the gas
as a whole, and not a true case of diflusion. The third method occurs
when the pores are exceedingly fine, such as those found in plates of
meerschaum, stucco, or a plate of graphite prepared by squeezing together
powdered graphite until it forms a coherent mass. In this case, when we [
have a mixture of two gases, each finds its way through the plate /
independently of the other, and the composition of the mixture is in I
general altered by the passage of the gas through the plate. The laws /
governing the passage of gases through pores of this kind were investi-
gated by Graham, who found that the volume of the gas (estimated at a
standard pressure) passing through a porous ^late was directly propor-
tional to the difference of the pressures of the gas on the two sides, and
inversely proportional to the^qiiare jroot of f he^molecular weight of J.he
gas^ Thus for the same diflerence of pressure hydrogen was found to
escape through a plate of compressed graphite at four times the rate of
^
202
propi:rties of matter.
oxygen. Thus, if we have mixtures of equal volumes of hydrogen and oxygen
and allow them to pass through a porous diaphragm, since the hydrogen
gets througli at four times the rate of the oxygen, the mixture, after pass-
ing through the plate, will be much richer in hydrogen than in oxygen.
The rate of diffusion can be measured by an instrument of the following
kind (Fig. 155) : A porous plate is fastened on the top of a tube which can
be used as a barometer tube. A vessel for holding the gas being attached
to the upper part of the tube, this and the space above the mercury are
exhausted ; gas at a definite pressure is then let into the vessel, and the
rate at which it passes through the diaphragm into the vacuum over the
mercury is measured by the rate of
depression of the mercury column.
The laws of diffusion of gases
through fine pores are readily explained
by the Kinetic Theory of Gases ; for if
the pores are so fine that the molecules
pass through them without coming
into collision with other molecules, the
rate at which the molecules pass through
will be proportional to the average
velocity of translation of the molecules.
According to the Kinetic Theory of
Gases this average velocity is inversely
proportional to the square root of the
molecular weight of the gas and directly
proportional to the square root of the ab-
solute temperature. Hence at a given
temperature the velocity with which
the gas streams through the apertures
will be inversely proportional to the
square root of the molecular weight ;
this is the result discovered by Graham.
Thermal Effusion. — The same
reasoning will explain another pheno-
menon sometimes called thermal effu-
sion. Suppose we have a vessel divided
nto two portions by a porous diaphragm ; let the pressures in the two
portions be equal but their temperatures different, then gas will stream
from the cold to the hot part of the vessel through the diaphragm. For
since the pressures are equal the densities in the two paits of the vessel
are inversely proportional to the absolute temperatures while the velocities
are directly proportional to the square roots of the absolute temperatures.
Hence the number of molecules passing from the gas through the
diaphragm, which is proportional to the product of the density and tho
velocity, will be inversely proportional to the square root of tho absolute
temperature; thus more gas will pass from the cold side than from the
hot, and there will be a stream of gas from the cold to the hot portion
throu<ih the dianhrafjm.
Atmolysis. — The diffusion of gases through porous bodies was applied
by Graliam to produce the separation of a mixtui^e of gases ; this
separation was called by him atmolYsis, and to efVect it he used an
instrument of the kind shown in 'Fiix. 15G. A long tube made from the
Fig. 15».
DIFFUSION OF GASES.
203
stems of clay tobacco-pipes is fixed by means of corks in a glass or
metal tube. A glass tube is inserted in one of the end corks, and is
connected with an air-pump so that the annular space between the
tobacco-pipes and the outer tube can be exhausted. The mixed gases
whose constituents have to be separated is made to flow through the clay
pipes. Some of tlie gases escape through the walls and can be pumped
away and collected while the rest flows on through the tube. In the gas
which passes through the walls of the tube there is a greater proportion
of the lighter gas than there was in the mixture originally, while in the
gas which flows along the tube there is a greater proportion of the
Fig, 156.
heavier constituent. If the constituents of the mixture differ much in
density a considerable separation of the gases may be produced by this
arrangement.
Passagre of a Gas through India-rubber. — The fact that gases
can pass through thin india-rubber Avas discovered in 1831 by Mitchell, who
found that india-rubber toy-balloons collapsed sooner when inflated with
carbonic acid than with hydrogen or air, and sooner with hydrogen than
air. The subject was investigated by Graham, who gave the following
table for the volumes of difierent gases which pass through india-rubber
in the same time :
CO
Air
CH.
1
11 3
1-149
2-148
0.
CO,
2-556
5-5
13-585
The speed with which the gases pass through the rubber increases
very rapidly with its temperature. There is no simple relation between
these volumes and the densities of the gas as there is in the case of
diffusion through a porous plate, and the mechanism by which the gases
effect their passage is pi'obably quite different in the two cases. The
passage of gases through rubber seems to have many points of resem-
blance to the passage of liquids through colloidal membranes such as
parchment-paper or bladder. The rubber is able to absorb and retain a
certain amount of_carbonic acid gas,_this^^inount increasing with the
pressure of the gas in contact with the surface of the rubber. Thus the
layers^ of^'ubber next the CO^ first get saturated with the gas, and this
state of saturation gets transmitted from layer to layer ; but as on the
other side of the sheet of rubber the pressure of the CO., is less, the outer
layei's cannot retain the whole of their COg so that some of the gas
gets free.
Passag-e of a Gas through Liquids.— This is probably analogous
to the last case ; the gases which are most readily absorbed by the liquid
are those which pass through it most rapidly.
204
PROPERTIES OF MATTER.
Passag'e of Gases throug-h red-hot Metal.— Deyille and Troost
found that hydrogen passed readily tlirough red-liot platinum and iron.
No gas besides liydrogen is known to pass through platinum. Troost
found that oxygen diil'used through a red-hot silver tube ; quartz is said
to be penetrable at high temperatures by the gases from the oxy hydrogen
flame.
Diffusion of Metals through Metals. — Daniel! showed that
mercury diffused through lead, tin, zinc, gold, and silver, Henry proved
the dif fusion of mercury through lead by a very striking experiment : he
took a bent piece of lead and placed the lower part of the shorter arm in
contact with mercury ; after the lapse of some time he found that the
mercury trickled out of the longer arm. He also showed the diffusion of
two solid metals thi'ough each other by depositing a thin layer of silver
on copper ; when this was heated the silver disappeared, but on etching
away the copper surface silver was found. A remarkable series of ex-
periments on the diffusion of metals through lead, tin and bismuth has been
made by Sir W. Roberts- Austen*; his results are given in the following
table. K is the diffusivity :
DifYusing Metal.
Solvent. Temperature.
K cm.7sec.
Gold
Lead
492° ...
3-47 X 10-5
9? * • •
>» ••
492° ...
3-55 X 10-5
Platinum
»>
492° ...
1-90x10-5
,, * * *
»
492^ ...
l-96xl0-»
Gold
5J
555 ...
3-G9xl0-5
J) ...
Bismuth
555 ...
5 23x10-5
,, • • •
Tin
555 ...
5-38x10-5
Silver
>> • •
555
4-77x10-5
Lead
5>
555
3-68x10-5
Gold
Lead
550 ...
3-69 X 10-5
Illiodium
5>
550 ...
3-51x10-5
It will be seen from these results that the rate of difl^usion of gold
through lead at about 500° is considerably greater than that of sodium
chloride through water at 18° C. Sir W. Roberts-Austen has lately shown
that there is an appreciable diffusion of gold through solid lead kept at
ordinary atmospheric temperatures.
• Roberts-Austen, .PAtZ. Trans. A., 1896, p. 393.
CHAPTER XVIII.
VISCOSITY OF LIQUIDS. '""^
Contents.— Definition of Viscosity — Flow of Liquid through Capillary Tube— Flow
of Gas throiisrh Capillary Tube— Metliods of Measurement of Co-efficients of
Viscosity — Effect of Tcrupcrature and Trcssurc on Viscosity of Liquids — Vis-
cosity of Solutions and Mixtures— Lubrication — Explanation of Viscosity of
Gases on Kinetic Theory — Mean-free Path— Efi'ects of Temperature and Pressure
on Viscosity of Gases— Viscosity of Gaseous Mixtures— Eesistance to Motion
of a Solid through a Viscous Fluid.
A FLUID, whether liquid or gaseous, when not acted on by external
forces, moves like a rigid body when in a steady state of motion. When
in this state there can be no motion of one part of the liquid relative
to another ; if such relative motion is produced, say by stirring the
liquid, it will die away soon after the stirring ceases. Thus, for example,
I when a stream of water flows over a fixed horizontal plane, since the
top layers of the stream are moving while the bottom layer in contact
with the plane is at lest, one part of the stream is moving relatively
to the other, but this relative motion can only be maintained by the
action of an external foi'ce which makes the pressure increase as we go
up stream. If this force were withdrawn the whole of the stream
A . B
C D
Fig. 157.
would come to rest. The slowly moving liquid near the bottom of
the stream acts as a drag on the more rapidly moving liquid near the top,
and there are a series of tangential forces acting between the horizontal
layers into which we may suppose the stream divided ; thus the foi ce
acting along a surface such as AB tends to retard the more rapidly
moving liquid above it and accelerate the motion of the liquid below
it ; it thus tends to equalise the motion, and if there were no external
forces These^ tangential ^stresses ^would soon reduce the fluid to rest.
The property of a liquid whereby it resists the relative motion of its
parts iscalled viscosityT TheTawof tEis viscous resistance was formu-
lated by JSewton {^frincijna, Lib. II., Sec. 9). It may be stated as
follows : Suppose that a stratum of liquid of thickness c is moving
horizontally from left to right and that the horizontal velocity, which
is nothing at CD, increases uniformly with the height of the liquid,
and let the top layer be moving with the velocity V ; then the
tangential stress which may be supposed to act across each unit of a
surface such as AB is proportional to the gradient of the velocity — i.e.,
to Y/c — and tends to stop the relative motion, the tangential stress on the
liquid below AB being fiom left to right, that on the liquid above AB
from right to left. The^ratio of the stress to the velocity^radient is called
the co-efiicient of viscosity of the fluid ; we shall denote it by the sym-
bol i{. The viscosity may be defined in terms of quantities, which may be
directly measured as follows : " The viscosity of a substance is measured
206 PROPERTIES OF MATTER.
by the tangential force on unit area of either of two horizontal planes
at unit distance apart, one of which is tixed, while the other moves
with the unit of velocity, the spa^e between being filled with the viscous
substance" (Maxwell's Them-y of Hcat).j'/) 'V^^-S'.
It will be seen that there is a close analogy between the vLscous
stress and the shearing stress in a strained elastic soUd. If a stratum
of an elastic solid, such as that in Fig. 157, is strained so that the hori-
zontal displacement at a point P is proportional to the height of P
above the plane CD, the tangential stress is equal to n x (gradient of
the displacement) where n is the rigidity of the substance. The viscous
stress is thus related to the velocity in exactly the same way as the
shearing stress is related to the displacement. This analogy is brought
out in the method of regarding viscosity introduced by Poisson and
Maxwell. According to this view, a viscous liquid is regarded as able
to exert a certain amount of shearing stress, but is continually breaking
down under the influence of the stress. \Ye may crudely represent
the state of things by a model formed of a mixture of matter in
states A and B, of which A can exert shearing stress while B cannot,
while under the influence of the stress matter is continually passing
from the state A to the state B. If the rate at which the shear
disappears from the model is proportional to the shear, say X0, where
0 is the shear, then, when things are in a steady state, the rate at
which unit of volume of the substance is losing shear must be equal
to the rate at which shear is supplied to it. If ^ is the horizontal
C displacement of a point at a distance x from the plane of reference, then
A d = —. The rate at which shear is supplied to unit volume is dd/dt or J^ :
■•je dx ^^ —!— dx dV
— but d^\dt is equal to «, the horizontal velocity of the particle, hence the
rate at which the shear is supplied is dvjdx. Thus, in the steady state,
dx
If n is the coeflScient of rigidity, the shear 0 will give a tangential
stress equal to nQ or
n dv
X dx.
If q is the coefficient of viscosity, the viscous tangential stress is equal to
dv - '--^ . - ^„-;.-x:-?:a*A
Hence, if the viscous stress arises ^ora_the rigidity ofthe_substance|^
7J = W/X.
The quantity 1/X is called the time of relaxation of the medium ; it
measures the time taken by the shear to disappear from the substance
when no fresh shear is supplied to it.
-V This view of the viscosity of liquids is the one that naturally suggests
itself when we approach the liquid condition by starting from the solid
state ; if we approach the liquid condition by starting from the gaseous
state we ai-3 led (see p. 218) to regard viscosity as analogous to diflfusion
VISCOSITY OF LIQUIDS.
«o7
And. as ai'ising from the movement of the molecules from one part of the
Eubstance to another. This jioint of view will be considered later.
Flow of a Viscous Fluid through a Cylindrical Capillary
Tube. — When the fluid is driven through the tube by a constant
dillerence of pressure it settles down into a steady stsite of motion such
that each particle of the fluid moves parallel to the axis of the tube,
'provided that the velocily of
the fluid through the tube does
not exceed a certain value de-
pending on the viscosity of the
liquid and the radius of the
tube. The relation between
the diflTerence of pressure at
the beginning and end of the
tube and the quantity of liquid
flowing through the tube in
unit time can be determined as
follows :
Let the cross-section of the
tube be a circle of radius OA = a,
let V be the velocity of the fluid
parallel to the axis of the tube
at a point P distant r from this
axis. Then dv/dr is the gradient
of the velocity, and the tangen-
tial stress due to the viscosity
is rjdv/dr: this stress acts paralltl
to the axis of the tube. Consider the portion of fluid bounded by two
coaxial cylinders through P and Q and by two planes at right angles to
the axis of the tube at a distance Az apart. Let r, r + Ar be the radii of
the cylinder through P and Q respectively. The tangential stress due to
viscosity acting in the direction to diminish v is at P equal to n— ; the
dr
area of the surface of the cylinder through P included between the two
planes is 2TrrAz, hence the total stress on this surface is
2nt]r-—Az
dr
Similarly the stress acting on the surface of the cylinder through Q
ipcluded between the two planes is
2nr,!y^ + ^(r'^]Ar\Az IT. ^^
( dr dr\ dr J J
and this acts in the direction to increase v; hence the resultant stress
Fio. 1.08.
-'V
r A^^
tending to increase v is equal to
27rr]—(r—-]ArAz
dr\ dr I
'J/y. yol^^
-6tc-*£.<
Besides these tangential forces there are the pressures acting over the
plane ends of the ring; if 11 denote the pressure gradient — i.e., the
increase of pressure per unit length in the direction of v. then the
208 PROPERTIES OF MATTER.
effect of the pressui'es over the ends of the ring is equivalent to
a force 2TrrAr.llAz tending to dimini.sh v. Since the motion is steady there
is no change in the momentum of the fluid, hence the force tending to
diminish v must be equal to that tending to increase it ; we thus get
dr\ dr J
Now since the liquid is moving parallel to the axis of the tube the
pressure must be the same all over a cross-section of the tube; hence
IT does not depend upon r. Again, v must be the same for all points
at the same distance from the axis, if the fluid is incompressible, for if
V changed as we moved parallel to the axis down the tube, the volume of
liquid flowing into the ring through P and Q would not be the same as
that flowing out. Since IT does not depend upon r, and the left-hand side
of equation (1) does not depend upon anything but r, we see that n must
be constant ; hence, integrating (1), we get •
dr ~
where C is a constant ; we have therefore
dr r
Integrating again we have
VV = |>-n4-0 1ogr-t-C' (2)
where C is another constant of integration. Since the velocity is not
infinite along the axis of the tube — i.e., when r = 0, 0 must vanish. To
determine C we have the condition that at the surface of the tube
the liquid is at rest, or that there is no slipping of the liquid past
the walls of the tvxbe. This has been doubted ; indeed, Helmholtz and
Piotrovvski thought that they detected finite efl'ects due to the slipping
of the liquid over the solid. Some very careful experiments made by
Whethani seem to show that under any ordinaiy conditions of flow no
appreciable slipping exists, at least in the case of liquids. We shall
assume then that ■?; = 0 at the surface of the tube — i.e., v/hen r — a; this
condition reduces equation (2) to
,v = |(r2-a2)n (3)
Now if pj is the pressure where the liquid enters the tube, p^ the
pressure where it leaves it, I the length of the tube,
11= -
{P^ - 2^2)
the negative sign is taken because the pressure gradient was taken
positive when the pressure increases in the direction of v. Substituting.
this value for 11, equation (3) becomes
rjv==^-^p{d--r^) (4)
VISCOSITY OF LIQUIDS.
20&
The volume of liquid Q which passes in unit time across a section of
the tube
a
-f
2Trrvdr.
OlT)
(5)
This is the law discovered by Poiseuille for the flow of liquids through
capillary tubes. We see that the quantity flowing through such a tube
isj)roportional to the square of the^areaTofcross-section of the tube^
When the liquid flows through the capillary tube from a large vessel,
as in Fig. 159, the pressui'e p^ at the orifice A of the capillary tube
diflers slightly from that due to the head of the liquid above A, for this
B
Fio. 159.
head of liquid has not merely to drive the liquid through the capillary
tube against the resistance due to viscosity, it has also to communicate
velocity and therefore kinetic energy to the liquid, so that part of the
Eead is used to set the liquid in motion. We can calculate the cor-
rection due to this cause as follows ; let h be the height of the surface
of the liquid in the large vessel above the outlet of the capillary tube, p
the density of the liquid ; then if Q is the volume of the Hquid
flowing through the tube in unit time, the work done in unit time is
equal to gpIiQ. This work is spent (1) in driving the liquid through the
capillary tube against viscosity, and this part is equal to (^J, -/>,) Q ^^
j3, and p^ are the pressures at the beginning and end of the capillary tube
(2) in giving kinetic energy to the liquid. The kinetic energy given to
the liquid in unit time is equal to
h
/"'
xvx 2Trrdr
Vrt *
'(.
where v is the velocity of exit at a distance r from the axis of the capillary
tube. If we assume that the distribution of velocity given by equation (4)
holds right up to the end B of the tube, then by the help of the equation (5)
we have
. / s-
210 PR0P]:RTIES OF MATTER.
Substituting this value in the integral we find that the kinetic ehebgy
possessed by the fluid issuing from the tube in unit time is pQ^Tr-a*;
hence, equating the -work spent in unit time to the kinetic enei'gy gained
plus the work done in overcoming the viscous resistance, we have
77 a
or 9l>[h--^]=2\-2^,
Thus the head which is spent in overcoming the viscous resistance is not h,
but h-
■K-a^g
This correction has been investigated by Hageubach,* Couette,t and
"Wilberforce,t and has been shown to make the results of experiments
agree more closely with theory. It is probably, however, not quite accu-
rate on account of the assumption made as to the distribution of velocity
at the orifice.
Viscosity of Gases. — The viscosity of gases may be measured in
the same way as that of liquids, but the case of a gas flowing through a
capillaiy tube differs somewhat from that investigated on p. 208, where
the liquid was supposed incompressible and the density constant ; in the
case of the gas the density will, in consequence of the variation in
pressure, vary from point to point along the tube. Using the notation of
the previous investigation, instead of v being constant as we move parallel
to the axis of the tube, the fact that equal^masses pass each cross-section
requires pv to be constant as long as we keep at a fixed distance from the
xxis'of the^libe. Since p is propoitional to />, where p is the pressure of
the gas, we may express this condition by saying that ^>w must be
independent of z where 2; is a length measured along the axis of the tube.
Thus, since p varies along the tube, v will not be constant as z changes ;
this variation of v will introduce relative motion between parts of the gas
at the same distance from the axis of the tube, and will give rise to
viscous forces which did not exist in the case of the incompressible liquid.
We shall, however, neglect these for the following reasons : if Y„ is the
greatest velocity of the fluid, the gradient of velocity along the tube is of
the oi'der "Vjl, where I is the length of the tube ; the gradient of velocities
across the tube is of the order V^/a, where a is the radius of the tube ; as
a is very small compared with I, the second gradient, and therefore the
viscous forces due to it are very large compared with those due to the first,
Weshall therefore neglect the effect of thefirat gradient. On this supposition
equation (1) still holds, and, since 11 = — , we have
dz
— I ^^- -17= -^
dr\ dr) dz
•
Hagenbach, Poggendorff's Annalen, 109, p. SS5.
t Conette, AnnaJcs de Chimic ct de Physique, [6], 21, p. 433
X Wilberforce, Philosophical Magazine, (5) 31,"p. 407.
VISCOSITY OF LIQUIDS. 2ii
Of, reo'arding ^; as constant over a cross-section of the tube, we have
dr\ dr
Since pv is independent of z, we see
that ^^' is constant and equal to
dz
Fig. 160.
Solving the differential equation in the same way as that on p. 208. re get
J. J..
212 PROPERTIES OF MATTER.
and if Y^ is the volume entering, V, that leaving the tube per second, w»
have
Measurement of the Coefficient of Viscosity.— The viscosity ij
has must frequently been determined by measurements of the rate of flow
of the iluid through cajiillary tubes. An apparatus by which this can be
done is shown in Fig. IGO. G is a closed vessel containing air under
pressure; the pressure in this vessel is kept constant by means of the tube
I>, which connects G with a Mariotte's bottle ; the pressure in G is always
that due to a column of water whose height is the height of the bottom of
the air tubes in the Mariotte's bottle above the end of the tube U. The
glass vessel abcdef, in which de is a capillary tube, contains the fluid whose
coefficient of viscosity is to be determined ; this vessel communicates with
i^
•[^ " , , "A^^Jf^^-^
Fig. 161. FiG. 162.
G by means of the tube LKI ; the pressure acts on the liquid in ahcdef,
and causes it to flow through the capillary tube from left to right ; two
marks are made at b and c, and the volume between these marks is
carefully determined. Let us call it V ; then, if T is the time the level of
the liquid takes to fall from h to c, Q = V/T. The area of cross-section of
the tube has to be determined with great care, and precautions must be
taken to prevent any dust getting into the capillary tube. As the
viscosity varies very rapidly with the temperature, it is necessary to
maintain the temperature constant; for this purpose the vessel aZ^cc^e/ is
placed in a bath filled with water.
With an apparatus of this kind Poiseuille's law can be verified, and
the viscosity determined. It is found that, although Poiseuille's law holds
with great exactness when the rate of flow is slow, yet it breaks down
when the mean velocity Q/7ra^ exceeds a certain value depending on the
size of the tube and the viscosity of the liquid. This point has been
investigated by Osborne Reynolds, who finds that the state of flow we
have postulated in deducing Poiseuille's law — i.e., that theJig[iud_moves in
straight linesparallel to the axis of the tube — cannot exist when the niean
vetocity exc&eusjTmt^ the steady flow is then replaced by an
irregular turbulent motion71;he particles of liquid moving from side to side
of the tube. This is beautifully shown by one of Reynolds' experiments.
Water is made to flow through a tube such as that shown in Fig. IGl, anda
little colouring matter is introduced at a point at the mouth of the tube : if
the velocity is small the coloured water forms a straight band parallel to
the axis of the tube, as in Fig. 161 ; when the velocity is increased this band
becomes sinuous and finally loses all defiuiteness of outline, the colour
filling the whole of the tube, as in Fig. 1G2. Reynolds conckided from his
(experiments that the^ steady^motion cannot exist if the mean velocity is
greater than 1000 rj/fM where t] is the viscosity, p the density oFthe Tiquid,
and a tlie radius ofThe tube. The units are centimetre, gramme and second.
Measurements of the viscosity of fluids both liquid and gaseous, have been
VISCOSITY OF LIQUIDS.
213
made by detei'mining the couple which must be apph'ed to a cylinder to
keep it fixed when a coaxial cylinder is rotated with uniform velocify, the
space between tlie cylinders being filled with the liquid whose viscositr
has to be determined. This method has been used by Couette and Mallock.
The theory of the method is as follows : the particles of the fluid will
describe circles round the common axis of the cylinders. Let PQ be points
on a radius of the cylinders;
after a time T, let P come to P',
Q to Q', let OP' produced cut QQ'
in Q". Then the velocity gradient
at P will be equal to {Q'Q"IT)^
P'Q" ; if w is the angular velocity
with which the particle at P de-
scribes its orbit, w + 3w that of the
particle at Q, then Q'Q" = OQ'cwT.
liBt OP = r, OQ — r + cr, then since
P'Q" = cr the velocity gradient at
P is (r + h')^^, or when h' is very
07'
small, r-~ ; hence the tangentiol
dr
stress acting on unit area of the
surface at P is nr—-. Now consider
dr
Fig. 1G3.
the portion of liquid bounded by
coaxial cylinders through P and R and by two parallel planes at right
angles to the axes of the cylinders and at unit distance apart. This
annulus is rotating with constant angular velocity round the axis of the
cylinders, hence the moment about this axis of the forces acting upon the
annulus must vanish. Now the moment of the forces acting on the inner
face of this annulus is
o d(o o -.db) - ^^'
Znri]y^r = ^nr]r*-z-
, dr dr
and this must be equal and opposite to the moment of those acting on the
outer surface of the cylinder; now E may be taken anywhere; hence we
see that this expression must be constant and equal to the moment of the
couple acting on unit length of the outer cylinder, which is, of course, equal
and opposite to the moment of that on the inner. Let us call this moment
r, then
Integrating this equation we find
2nrjr^^=r
dr
to)= —
4iTrT]r'-
+ 0
■where C is a constant. If the radii of the inner and outer cylinders are
a and b respectively, and if the inner cylinder is at rest and the outer one
rotates with an angular velocity Q, then since w = 0, when r = a, and w = i2
when r = b, we find
07 O
0- -a^
214 PROPERTIES OF MATTER.
Hence, if we measure r for a given velocity il, we can deduce the value of tf.
This case presents the same peculiarities as the flow of a viscous liquid
through a capillary tube ; the law expressed by the preceding equation is
only^beyed when Ci, is less than a cei'tain critical valua When £1 exceeds
this value the motion of the fluid becomes turbulent, and for values of Q,
just above this value the relation between r and il becomes irregular ; it
becomes regular again when i2 becomes considerably greater , but r is no
longer proportional to il, but is of the form ai^ 4- 0Qi- where a and ft are
constants. These facts are well shown by the curve given in Fig. 164,
/
/
/
/
I
I
I
t
r
-' B
XI
Fio. 164.
which represents the results of Oouette's* experiments on the viscosity of
water. The abscissae are the values of Q, and the ordinates the values
of r/li. The instability set in at B when the outer cylinder made about
one revolution per second ; the radii of the cylinders were 14*64 and 14'39
cm. respectively.
This method can be applied to determine the viscosity of gases as well
as of liquids.
Method of the Oscillating' Disc. — Another method of determining
T}, Avhich has been used by Coulomb, Maxwell, and O. E. Meyer, is that of
measuring the logax-ithmic decrement of a horizontal disc vibrating over a
fixed parallel disc placed at a short distixnce away, the space between the
discs being filled with the liquid whose viscosity is required. The viscosity
• Couette, Annales de Chimie et de Physique [6], 21, p, 433.
VISCOSITY OF LIQUIDS.
215
of the liquid gives rise to a couple tending to retard the motion of the
disc proportional to the product of the angular velocity of the disc and
the viscosity of the ligmd : the calculation of this couple is somewhat
difficult. We shall refer the reader to the solution given by Maxwell
1Z00
iBoa
woa
I
uoo
900-^
700-
500 i
300
GO eo 70
TeTTiper^ttiine
Fig. 166.
{Collected Paj-ers, vol. ii. p. 1). This method, as well as the preceding one,
can be used for gases as well as for liquids.
Among other methods for measuring rj we may mention the determina-
tion of the logarithmic decrement for a pendulum vibrating in the fluid
(Stokes) ; the logarithmic decrement of a sphere vibrating about a diameter
216
PROPERTIES OF MATTER.
iu an ocean of the fluid ; the logarithmic decrement of a hollow sphere
filled with the liquid and vibrating about a diameter (Helmholtz and
Piotrowski, Helmholtz Collected Papers, vol. i. p. j 72).
Temperature Coefficient of Viscosity. — In all experiments on
viscosity it is necessary to pay great attention to the measurement of the
temperature, as the coefficient of_yiscosity^ of liquids dim^ishes vei-y
rsyDicUy^as ilie_jtemperature jnerei^ This is shown by the curve (Fig.
Ibojiaken from the paper by Thorpe and Rodger [Phil. Trans., 1894, A.
Part ii. p. 397), which shows the relation between the viscosity of water
and its temperature. It will be seen that the viscosity of water at 80° C.
is onl}' about one-third of its value at 10° 0. Thorpe and Rodger, who
determined the co-efficients of viscosity of a large number of liquids, found
tlie formula given by Slotte, ?; =0/(1 + ii)", where rj is the co-efficient of
viscosity at the temperature t and U, h and n are constants depending on
the nature of the liquid, was the one that agreed best with their experi-
ments. For water they found that
•017941
(1 + •02312001-
biXZ
where t is the temperature in degrees Centigrade.
The following table, taken from Thorpe and Rodger's paper {Phil.
Trans., A. 1894, p. 1), gives the value of i^ in C.G.S. units for some liquids
of frequent occurrence. The table gives the value of the constants (J, 6, n
in Slotte's formula
, = C/(l+5i)»
Substance
0
h
n
Bromine
•012535
■008935
1-4077
Chloroform .
■007006
•006316
1-8196
Carbon tetrachloride
•013466
•010521
1-7121
Carbon bisulphide
•004294
•005021
1-6328
Formic acid
•029280
•016723
1-7164
Acetic acid .
•016867
•008912
2-0491
Ethyl ether
•002864
•007332
1-4644
Benzene
•009055
•011963
1-5554
Toluene
•007684
•008850
1-6522
Methyl alcohol .
•008083
•006100
26793
Ethyl alcohol . . .
•017753
•004770
4-3731
Propyl alcohol
•038610
•007366
3-9188
Butvl alcohol :
6° to 52° ....
•051986
■007194
4-2452
52° to 114°
•056959
■010869
32150
Inactive amyl alcohol :
0°to40°
•085358
■008488
4-3249
40° to 80° ... .
•093782
•012520
3-3395
80° to 128°
•152470
•026540
24618
Active amyl alcohol :
0°to35°
•111716
■009851
4-3736
35° to 73°
•124788
•015463
3-2542
73° to 124°
•147676
•127583
2 0050
Allyl alcohol
•021736
•009139
2-7925
Nitrogen peroxide ....
■005267
■007098
1-7349
VISCOSITY OF LIQUIDS. 217
"Warburg found that rj for mercury at 17"2° is equal to •016329. A later
determination by Umani (iY?fo?'. Cim. [4] .3, p. 151) gives »; = "01577at 10°.
Tlie value of t; for liquid carbonic acid is very small, being at 15° only
1/14-6 of that of water.
Effect of Pressure on the Viscosity. — The viscosity_pf water
diminishes slightly under_jiicreased pressure, while~that ofbenzol and
ether^increases^
Viscosity of Salt Solutions. — A large number of experiments
have been made on the viscosity of sohitions, but no simple laws con-
necting the viscosity with the strength of the solution have been arrived
at. In some cases the viscosity of the solution is less than that of water,
and in many cases the viscosity of the solution is a maximum for a particular
strength.
Viscosity of Mixtures. — Here again no general results have been
arrived at, although considerable attention has been paid to this subject.
In many cases the viscosity of a mixture of two liquids A, B is less than
that calculated by the foi-mula
7 =
a + b
where rix, Vb ^^^ respectively the viscosities of A and B, and a, h are the
volumes of A and B in a volume a + b of the mixture.
Lubrication. — When the surfaces of two solids are covered with oil
or some other lubricant they are not in contact, and the friction between
them, which is much less than when they are in contact, is due to fluid
friction. The laws of fluid friction discussed in this chapter show that,
iFweTiave two parallel planes at a distance d apart, the interval between
them being filled with a liquid, then if the lower plane is at rest and
the upper one moving parallel to the lower one with the velocity V,
if V is not too great there is a retarding_tang^ntial force acting on_the
moving plane, and equal per unifarea to TfYjd, where 17 is a quantity
called the coefficient of^viscosity^oFThe liquid. If we regard this as a
frictional force acting on the moving plate we see that the friction would
depend upon the velocity, and would only depend upon the pressure between \
the bodies in so far as the pressure afiected the thickness of the liquid \
layer and the viscosity of the lubricant.
The laws of friction, when lubricants are used, are complicated, depending
largely upon the amount of lubrication. When the lubricant is present
in sufficiently large amounts to fill the s-paces between the moving parts
the friction seems to be proportional to the relative velocity of these parts.
When the supply of lubiicant is insufficient, part of it collects as a pad
between the moving parts, as in Fig. 166; here the lower surface is at
rest and the upper one rotating from left to right. Professor Osborne
Reynolds* has shown that, as the breadth and thickness of this pad
depend upon the pressure and relative velocity, it would be possible to get
friction proportional to the pressure and independent of the relative
velocity, even when the friction was entirely caused by the viscosity of a
thin layer of liquid between the moving parts.
Viscosity of Gases. — Gases possess viscosity, and the forces called
into play by this property are, as in the case of liquids, proportional to
the velocity gradient ; in fact, the definition of viscosity given on p. 205,
* Reynolds, Phil. Trans., 1886, pt. i. p. 157.
218 PROPERTIES OF MATTER.
applies to gases as well as to liquids. The most remarkable property of
the_viscosity^_gases is that within jvvide limits of pressure the viscosity
is indepemTent of the pressure, being under ordinary circumstances the
same at a pressure of a few millimetres of mercury as at atmospheric
pressure. This is known as Maxwell's Law, as it was deduced by Maxwell
from the Kinetic Theory of Gases ; it has been verified by numerous
experiments. Boyle has some claim to be regarded as the discoverer
of this law, for about 1660 he experimented on the effect of diminishing
the pressure on the vibrations of a pendulum, and found that the vibrations
died away just as quickly when the pressure was low as when it waj
high. This law follows very readily from the view of viscosity supplied
by the Theory of Gases. Thus, suppose we have two layers of gas A
and B at the same pressure, and that A has a motion as a whole from
left to right, while B is either at rest or moving more slowly than A in
this direction. According to the Kinetic Theory of Gases, molecules of
the gas will be continually crossing the plane separating the layer A from
B
Fig. 167.
the layer B. Some of these molecules will cross the plane from A to B
and an equal number, since the pressure of the gas remains uniform, from
B to A. The momentum parallel to the plane of those which leave A
and cross over to B is greater than that of those which replace them
coming over from Bto A ; thus the layer A is continually losing momentum
^ while the layer B is gaining it. The effect is the same as if a force parallel
to the plane of separation acte3^on_ the layer ^17 so as to tend to
stop theliibtion from left to right, while an equal and opposite force acted
on B, tending to increase its motion in this direction ; these forces are
the viscous forces we have been discussing in this chapter. If the distri-
bution of velocity remains the same, the magnitude of these forces will
be proportional to the number of molecules which cross the plane^of sepa-
ration in unit time.
The molecules are continually striking against each other, the average
free run between two collisions, called the mean free path of the molecules,
being extremely smalTj only about 10^ cm. tor air, at txtmosplieric
pressure. This free path varies, however, inversely as the pressure, and at
the extremely low pressures which can be obtained with modern air- pumps
VISCOSITY OF LIQUIDS.
219
can attain a length of several centimetres. When one molecule strikes
against another its course is deflected, so that, although it is travelling at
a great speed, it makes but little progress in any assigned direction. The
consequence of this is that the molecules which cross in unit time the
plane of separation between A and B can all be regarded as coming from
a thin layer of gas next this plane, a definite fraction of the molecules
in this layer crossing the plane. The longer the free pfithj)f the molecules
the thicker the^ layer, the
\
tliickhess being directly
proportional to the mean
free path. If n is the
number of molecules per
unit volume and t the
thickness of the layer,
the number of molecules
which in unit time cross
unit area of the plane
separating A and B will
be proportional to nt.
Let us consider the efiect
on this numbsr of halvini?
the pressure of the gas.
This halves n but doubles
l< ; t is proportional to the
(free path, which varies
inversely as the pressure,
hence_the_prQdjict_2i4_and
therefore the .jviscosity,
' This
the
remains unaltered.
l(Ii~'until
rasoning
J
Milliont-hs of an Atmospheric •
Fig. 168.
thickness of the layer from
which the molecules cross
the plane of separation
gets so large that the layer
reaches to the sides of
the vessel containing the
gas. When this is the
case no further diminu-
tion^in Jihe ^essure can
increase t, and as n dimin-
ishes as the pressure
diminishes, the product
nt and, therefore, the viscosity, will fall as the pressure falls. Thus in a
vessel of given size the viscosity remains unaffected by the pressure until
the pressure reaches a certain value, which depends upon the size of the
vessel and the nature of ^theTg^fl wheinhis pressure is passed the
viscosity diniinisTies rapidly with the pressure. This is shown very clearly
by the curves in Fig. 168, based on experiments made by Sir William
Orookes {Phil. Trans., 172, pt. ii. 387). In these curves the ordinates
represent the viscosity and the abscisste the pressure of the gas.
The diminution in viscosity at low pressures is well shown by an incan-
descent electric lamp with a broken filament. If this be shaken while the
220
PROPERTIES OF MATTER.
lamp is exhausted it will be a long time befoi-e the oscillations die away;
if, however, air is admitted into the lamp through a crack made with a
file the oscillations when started die away almost immediately.
Another reason why the effects of viscosity are less at very low pressures
than at higher ones is the slipjiing of the gas over the surface^of t^e solids
with^ which it is in contact. In the case of liquids, no effects due to slip
have been detected. Kundt and Warburg* have, however, detected such
effects in gases even up to a pressure of several millimetres of mercury.
TheJaHZ-oL^slip {see Maxwell, " Stresses in a Rarefied Gas," Phil. Trans.,
187) may be expressed by saying that the motion in the gas is the same
as if a certain tjiickness L were cut off the solids, and that the gas in
contact vvithtliisjiew siw-face^were at restV Tbis thickness L is propor-
liionaTjtoJLhejgiean free path of the molecules of the^as. ^SccordTng to
the experiments of Kundt and Warburg it is equal to twice the free
path ; hence, as soon as the free path gets comparable with the distance
between the solids in the gas.
of
the slip
the same
the gas over
direction as
these solids will
a reduction in
produce appreciable eflects in
viscosity.
Mean Free Path. — If we know the value of the
calculate the mean free path of the molecules of a gas :
late, from the principles of the Kinetic Theory of Gases, the rate at which
momentum is flowing across unit area of the plane A, B, Fig, 167, we find
viscosity we can
for if we calcu-
that it is equal to
•350cpX^
where v is the velocity of the stratum at a height x above a fixed plane,
X is the mean^'free path, p the density of the gas, c the " velocity of mean
square" (this can be calculated from the relation ;j = |-pc- where jt> is the
pressure in the gas). The rate of flow of momentum across unit area
is equal to the tangential stress at the plane AB ; hence, if rj is the viscosity
of the ga«, T] — ' 350cpX. Let us calculate from this equation the value
of X for air ; taking for the viscosity at atmospheric pressure and at
15° C. j; = 1-9x10'^, p at pr-essure 10® and temperature 15° C,
1'2G X 10"^, we get c = i-yy x lU*, and X = -00001 cm. At the pressui-e of a
millionth j)f_juwitmospherejthejnean free path in air is 10 cm.
TEe^values^oF^/Tor^Tfewof the most important gases are given in
the following table ; the temperature is about 15° C. These numbers
are given by 0. E. Meyer ; they are deduced from his own experiments
on the viscosity of air by the method of the oscillating disc and the expe-
riments made by Graham on the relation between the rates of flow of
different gases thi'ough capillai-y tubes :
Gaa
T) X lOJ
Gas
>)X10<
Air .
. 1-9
Sulphuretted hydrogen
. 1-3
Hydrogen
. -93
Ilydrocliloric acid .
. 1-56
Marsh-gas
. 1-2
Carbonic acid .
. 1-6
Water-vapour .
■975
Nitrons oxide (NoO)
. 1-6
Ammonia
. 1-os
Methyl ether . " .
. 1-02
Carbonic oxide
. l-8i
Methyl chloride
. 116
Ethylene .
, 1-09
Cyanogen
. 1-07
Nitrogen .
. 1-84
Sulphurous acid (SO.,)
. 1-38
Oxygen .
. 2-12
Ethyl chloride
. 1-05
Nitric oxide (NO)
. 1-86
Chlorine . . .
. 1 41
Pugg. Ann., 155, p. 357.
VISCOSITY OF LIQUIDS.
221
Effect of Temperature upon the Viscosity of Gases.— Increase
_of temgeiatuie has opposite eliccts on the viscosities of liquids and oFgases,
for while, as we have seen, it diminishes tliejviscosity of liquids it increases
that of gases. If ?? is the coeiHcient of viscosity, and if this is assumed
to Fo proportional to T" where T is the absolute temperature, then, according
to Lord ilayleigh's* experiments, we have the following values for n :
Air .
Oxygen
Hydrogen
Helium
Areon .
n
•754
•782
•681
•681
•815
1113
128-2
72-2
72-2
150-2
The values of c relate to a formula suggested by Sutherland, according
T* ...
to which 7j = a n^ ; thus, at very high temperatures, if this relation
' 1+c/T'
is true, jj would vary as the square root of the absolute temperature.
According to Koch,t the viscosity of mercury vapour varies much more
rapidly with the temperature than that of any other known gas. He
concluded from his experiments that for this gas rj = aT''". The results
given above for helium and argon, both, like mercury vapour, monatomic
elements, show that a rapid variation with temperature is not a necessary-
characteristic of monatomic gases. Loi-d Eayleigh found that the viscosity
of argon was 1-21, and of helium 0"9G that of air.
Coefficient of Viscosity of Mixtures.— Graham made an extensive
series of experiments on the coeiiicients of viscosity of mixtures of gases
by meisuring the time taken by a known volume of gas to flow through
a capillary tube. He found that for mixtures of oxygen and nitrogen, and
of oxygen and carbonic acid, the rate of flow through the tubes of thej
mixture was the arithmeticaLmean rate of the gases mixed ; with mixtures
containing hydrogen the results were very diflferent ; how difterent is shown
by the following table, which gives the ratio of the transpiration time of
the mixtures to that of pure oxygon :
Hydrogen and Carbonic Acid.
4434
5282
5880
7488
8179
8790
8880
8960
900
It will be seen from this table that, while the addition of 5 per cent,
of air to pure hydrogen alters the time of eflusion by about 20 per cent.,
the mixture of half hydrogen, half air, has a time of effusion which only
diflfei's from that of pure air by about 8 per cent. Thus the addition of
hydrogen to air has little influence on the viscosity, while'~tITe~ addition
of~air to hydrogenrliaE^n enormous influence.
ResistaHct^cTarSolttlrTTrovli^^^ a Viscous Fluid.— When
a solid moves through a fluid the portions of the fluid next the solid are
* Kayleicb, Proc. Boy. Soc, 66, p. 68.
t Koch,^Wicd. Ann., 19, p. 587.
100
0
97-5 .
2-5
95
5
90
.. 10
75 .
.. 25
50
.. 50
25
.. 75
10
90
0
.. 100
Uydrogen
and Afr.
4321
100
0
4714
95
5
5157
90
. 10
5722
75 ..
25
6786
50
50
7339
25
. 75
7535
10
90
7521
5
95
•7470
0
. 100
222 PROPERTIES OP MATTER.
moving with the same velocity as tlie solid, while the portions of the fluid at
some distance ofi" are at rest. The movement of the solid thus involves
relative motion of_the fluid ; the viscosity oT the fluid resists tins motion,
so thatThereTs a force acting on the solid tending to resist its motion.
Sir George Stokes has shown tliat in the case of a sphere moving with
a very small uniform velocity V through the fluid the force resisting the
motion is equal to 67r>;ftV where a is the radius of the sphere, ri the
viscosity oT~the fluid through which it is falling. Consider now the case
of a sphere falling through a viscous fluid ; just after starting from rest the
velocity will be small and the weight of the sphere will be greater than
tne viscous resistance; the velocity of the sphere, and therefore the
i-esistance, will increase until the resistance is equal to the weight cf the
sphere. When this velocity, which is called the critical velocity, is reached,
the forces acting on the sphere will be in equilibriuna^ and Hie sphere \vill
fa]ljyvathjjmiiorm^elocit^^ the terminal velocity.
Since the effective weightoFThe^here is equal to~i7r<r(p - o-)^/3, where p is
the density of the sphere and o-that of the liquid through which it is moving,
if V is the terminal velocity,
6
or ^2gAp^ ^j^
so that the terminal velocity is proportional to the square of the radius
of the sphere. In the case of a drop of water falling through air for which
ij = 1"8 X 10"*, we find, if the radius "of the drop is 1/100 of a millimetre,
"V'= l'2cm^sec. This result explains the slow rate at^which clouds con-
sisting of fine drops of water fall. Since ri is independent of the pressure,
the terminal velocity in a gas will, since c in this case is small compared
"with p, be independent of tJ^^'p^^essure.
As an applicjxtion of this formula we may mention that the size of small
drops of water has been determined by measuring the rate at which they
fell through air ; from this the value of the radius can be determined by
equation (1). The expression for tlie resistance experienced by the sphere
falling through the viscous liquid is obtained on the supposition that the
motion of the liquid is so slow that terms depending upon the squares of
the velocity of the liquid can be neglected in comparison with those re-
tained. Now, if V is the velocity, p the density of the liquid, the forces on
the liquid depending upon the squares of the velocity, are proportional to
the gradient of the kinetic energy per unit volume — i.e., to the gradient of
^pV-; the forces due to viscosity are proportional to the gradient of the
viscous stress. If a is the radius of the sphere, the distance from the
sphere at which the velocity may be neglected is pio[)ortional to a, hence
the velocity gradient is of the order (V/a), and the viscous stress T)Yla.
Hence, if we can reject the effects depending on the squares of the
velocity in comparison with the effects of viscosity, pV^ must be small
compared with rfVja, or pVa must be small compared with rj. Hence, if
the preceding solution holds, we see, by substituting for V the value of
the limiting velocity, that -g—^ — ^—^ must be small. Lord Rayleigh *
'J jj-
* Lord Kajleigh, Phil. Ma<j., \b] 36, p. 354.
VISCOSITY OF LIQUIDS. go.'J
has pointed out how much this restricts the application of Stokes* result;
thus, for example, in the case of drops of water falling through air, the
theory does not apply if the drops are moi-e tlum about one-tenth of a
millimeti"e in radius. When the velocity of the falling body exceeds a
certain critical value the motion of the surrounding fluid becomes
turbulent, just as when the velocity of a fluid through a capillary tube
^exceeds a certain value the flow ceases to be regidar (see p. 212). When
this turbulent stage is reached the resistance beconiesjjroportional to the
8quare~of tKe velocity. Mr. Allen,* who has recently investigated the
resistance experienced by bodies falling through fluids, finds that this can
be divided roughly into three cases — (a) where the velocity is very small,
when the preceding theory holds, and tlie resistance is proportional to the
velocity ; (b) a stage where the velocity is great enough to make the forces
tiepending on the square of the velocity comparable with those depending
on viscosity ; in this stage the resistance is proportional to the velocity
raised to the power of 3/2 ; (c) a stage where the velocity is so great that
the motion of the fluid becomes turbulent ; in this stage he finds the
resistance to be projDortional to the square of the velocity. When the
resistance is proportional to the squai-e of the velocity the method of
dimensions shows that it does not for a given velocity depend upon the
viscosity of the liquid. For, suppose the resistance is proportional to
a'^p^ifY", this expression must be of the dimensions of a force — i.e., 1 in
mass, 1 in length, and — 2 in time ; hence we have
r>^'^4^ L^ ?=^+^ , y -^^^'
■ ^^' P^ l=x-^-z + n
x = n, y = n-l,z = 2-n,
and the resistance is prgportjonal to {^(i(i/rj)"{7]'/p); thus, if w = 2 the
resistance is proportional to Y^aFp, and~is independent of viscosity. The
energy of the body is spent in producing turbulent motion in the liquid
and not in overcoming the viscous resistance.
A great deal of attention has been given to the resistance of bodies
moving with high speeds, such as bullets. It is doubtful, however, if the
viscosity of the fluid tlu'ough which the bullet moves has any efiect upon
the resistance ; we shall not, therefore, enter into this subject, except to
say that the most recent researches, those by Zahm, seem to indicate that
for velocities less than about 30000 cm. /sec. the resistance may be repre-
sented by uv' + iy^, where a and h are constants.
* Allen, Phil. Mag., Sept. and Nov. 1900.
7--. _//
INDEX
Acceleration due to gravity, 7-24
Air, deviations from Boyle's law as to, 126
Airy, hydrostatic theory of earth's crust,
23
Dolcoath experiment, 35
Harton pit experiment, 35
Amagat, minimum value of pv., 126, 127
Angle of shear, 66
Arc, correction for pendulum swing, 10
Atmolysis, 202
Baily'S Cavendish experiment, 39
Bailie and Cornu's experiment, 39
Bars, bending of, 85-102
vibration of, 94
Barymeter, von Sterneck's, 26
Bending of rods or bars, 85-102
Cernouilli's correction for arc of swing
of pendulum, 10
Boiling-point, depression of, in solutions,
191
Borda's pendulum experiments, 10
Bouguer's pendulum experiments, 10
experiments on determination of
density of earth, 32
rule and exceptions, 22-3
Boyle's law, 125
at low pressures, 128
deviations of various gases from, 126
Boys's Cavendish experiment, 40
Braun's Cavendish experiment, 41
Breaking-point of stretched wires, 55
Bubbles and drops, measurement of
surface tension by, 156, 161
Camphor, movements of on surface of
water, 169
Capillarity, 135-181
Laplace's theory of, 173-181
Capillary tubes, rise of fluids in, 140
Carbonic acid, deviation of, from Boyle's
law, 126
Carlini's pendulum experiment, 35
Cassini's and Borda's pendulum experi-
ment, 10
Cavendish experiment, 36
by other observers, 39
see Earth, determination of density of
Clairaut's theorem, 22
Collision, 109
duration of, on impact, 112
of drops, 172
see also Impact
Colloids, 186
Compressibility of liquids, see Liquids
Computed times of pendulums, 15
Contamination of films, 170
Critical velocity in viscous fluids, 222
Crystalloids, 186
Defforges' pendulum, 19
Degree of latitude, measurement of a,
21
Diaphragm, diffusion through, 186, 200
Differential gravity balance, 26
Diffusion of gases, see Gases
of liquids, see Liquids
of metals, 204
Dilatation under strain, 64
Dissociation of electrolytes, 194
Earth, determination of density of, 31
by Airy, 35
Baily, 39
Buuguer, 32
Boys, 41
Braun, 41
Carlini, 35
Cavendish, 36
Cornu and Bailie, 39
von Jolly, 42
Maskelyne, 33
Mendenhall, 35
Poynting, 43
Richarz and Krigar-llenzel, 42
von Sterneck, 36
Wilsing, 41
Effusion, thermal, 202
Elastic after-effect, 55
curve, 95
fatigue, 57
limit, 53, 69
Elasticity, 53
modulus of, 69, 102
see also Young's Modulus
Electrolytes, dissociation of, 194
Ellipticity of earth, 23, 24
Elongation under strain, 64
226
INDEX
Equilibrium of liquids in contact, 139
Equivalent simple pendulum, 13
Fatigue, elastic, 57
Faye's rule, 23
Films, contamination of, 170
cooline; cflects, on stretching, 163
stability of cylindrical, 147
Flexure, 99
Floating bodies, forces acting on, 153
Fluid motion, effect of, on pendulums, 14
surfaces, disruption of, 174
Formulae for pendulum motion, 13-24
Freezing-point, depression of in solu-
tions, 193
Galileo's observations respecting pen-
dulums, 8
Gaseous pressures and volumes, 124
Gases, diffusion of, 196
kinetic theory as applied to the, 198
obstruction to, offered by perforated
diaphragms, 200
through porous bodies, 201
Gases, passage of, through india-rubber,
203
through liquids, 203
through red-hot metals, 204
Gases, viscosity of, 210, 218
influence of temperature upon, 221
Gravitation, constant, 29
Newton's law, 28
qualities of, 45-52
see also Earth, density of
Gravity, acceleration of, 7
history of research, as to, 7
Clairaut's theorem, 22
Newton's theory of, 20
Richer's observations on, 20
Swedish and Peruvian expeditions
of investigation, 21
Gravity balance, Threlfall and Pollock's,
27
Gravity meters, differential, 26
Half-seconds pendulum, von Sterneck,
24
Hodgkinson's table of values of e on
impact, 114
Homogeneous strain, 62
Hooke's law, 69
Hydrogen, deviations of, from Boyle's
law, 126
Hydrostatic theory, 23
Huygens' pendulum clock, 9
theory of pendulums, 9
Indian survey, experiments on pendu-
lums,'23
Impact, 109
duration of collision on, 112
kinetic energy of, 110
Invariable pendulum, 28
Jaeger's method of determining mean
surface-tension, 162
JoUv, von, experiments on gravitation
42
Kater's convertible pendulum, 12
and Sabine's experiments, 23
Kelvin's table of thermal effects ac-
companying strain, 134
Kinetic theory of gases, 218
explanation of diffusion by the,
198
Laplace's theory of capillarity, 173
Latitude, determination of length of 1'
of, 21
Liquids, capillarity of, 135
compressibility of, 116, 122
diffusion of, 183
determination of co-efEcient ol
184
through membranes, 186
in contact, 139
films, stability of, 147
flow of viscous, through cylindrical
capillary tubes, 207
potential enerey of, due to surface
tension, 137
rise of, in capillary tubes, 140
surface-tension of, 137
relation between curvature and
pressure of surface, 142
methods of measuring, 155
by bubbles and drops, 156, 161
by ripples, 157
temperature, effects on, 163
table of compressibility of various,
122
tensile strength of, 122
vapour-pressure over curved surface
of, 166
viscosity of, 205
Loaded pillar, stability of, 97
wires, anomalous effects in, 58
Lubrication, 217
Mass, 3
constancy of, 5
definition of, 4
unit of, 5
Maxwell's law of gaseous viscosity, 218
Mean free path, 218, 220
Mendenhall's gravitation experiment, 35
Mercury, compressibility of, 121
Metals, diffusion of, through metals, 204
elastic properties of, 53, 57
viscosity of, 57
Michell, I^lev. J., 36
Microstructure of metals under stress
58
Modulus of elasticity, 69, 102
Young's, 70, 73, 74, 76
of rigidity, 7
INDEX
227
Newton's theory of gravitation, 28
theory of gravity, 20
Nitrogen, deviation of, from Boyle's law,
126
Normal stress, 68
Oil, effect of, on waves, 171
Osmosis, 186
Osmotic pressure, 188
Pendulums, Bessel's experiments, 13
Borda and Cassini's, 10
clock, 9
Defforges, 19
formulas for, 13-24
Half -seconds pendulum, 24
Huygens' theory of, 9
Indian survey experiments, 23
invariable, 23
Kater's convertible, 12
Newton's use of, 9
Papers on the theory of, 7
Kepsold's, 18
von Sterneck's, 24
U.S. survey, 20
variation in length of seconds, 2
yielding of support of, 18
Permanent set, 53
Picard's pendulum experiments, 9
Piezometer (the), 119
Poiseuille's law, 209
Poisson's ratio, 73, 87, 120
Poynting's gravitation experiments, 43
Pressure, effect of, on viscosity, 217,
219
on volume, 124
variations from Boyle's law at low,
128
QUAETZ thread gravity balance, Threl-
fall's, 27
Reich's Cavendish experiment, 39
Repsold's pendulum, 18
Resolution of strain, 65
Reversible pendulum, theory of, 13
Reversible thermal effects accompanying
strain, 131
Richer, observations on gravity, 20
Rigidity, co-efficient of, 83
modulus of, 70
Ripples, measurement of surface-tension
by, 157
Rods, stresses and strains of, 71, 73, 79,
83, 85-102
Sabine's pendulum, 23
Salt solutions, viscosity of, 217
Schiehallion experiment, 32
Shear, 65
angle of, 66
Soap-bubbles, 143
Solutions, depression of boiling-point of,
191
of freezing-point of, 193
vapour pressure of, 190
Spiral springs, 101-108
energy of, 104-108
Stability of cylindrical films, 147
of loaded pillar, 97
Sterneck, von, Barjmeter, 26
half-seconds pendulum, 24
pendulum experiments, 36
Strain, 62
anomalous effects of alternating, on
wire, 58
alteration of micro-structure con-
sequent on, 59
axes of, 64
homogeneous, 62
resolution of a, 65
in relation to work, 70
thermal effects accompanying, 131
Stresses, 68
on bars, 71
Stretched film, 144
cooling due to stretching, 163
Stretched wire, anomalous effects on
loading, 58
Surface-tension, 137
effects between two liquids, 179
in thick films, 178
forces between 2 plates, due to, 152
Surface-tension, Jaeger's method of
measuring, 162
oscillations of a spherical drop
under, 160
of thin films, 164
measurement of by detachment of
a plate, 161
Ripple method, 157
Wilhelmy's method, 161
Swedish and Peruvian expeditions to
determine length of 1° of lati-
tude, 21
Table of moduli of elasticity, 102
thermal effects of strain, 131
Tangential stress, 68
Temperature, co-efficient of viscosity, 216
effects of, on surface-tension, 163
on breaking stress of wires, 61
Tensile strength of liquids, 123
Terminal velocity in viscous fluids, 222
Thermal effects of strain, 131
Kelvin's table of, 134
Thermal effusion, 202
Thickness of films, influence of, on
surface-tension, 178
Thin films, surface-tension of, 114
Threlfall and Pollock's gravity balance,
27
Torsion, 78
in cylindrical tubes, 78
in solid rods, 79
228
INDEX
U.S. Survey pendulums, 20
VArouR, diffusion of, 197
Vapour pressure, of solutions, 190
on curved surfaces, 166
Vibration of bars, 95
Viscosity, 60
temperature co-efficient of, 216
determination of co - efficient
212
by oscillating disc, 214
effects of pressure upon, 217
gaseous, effect of temperature
221
of gases, 218
of liquids, 205
of metals, 57
of mixtures, 221
of salt solutions. 21 7
of,
on,
Viscous fluids, resistance of, to motion of
solids, 221
velocity in, 222
Volume and pressure of gases, 124
Water, compressibility of, 121
Waves, calming of, by oil, 171
Weight, 1
standards of, 5
Wilhelmy's method of measuring sur-
face-tension, 162
Wilsing's gravitation experiments, 41
Work in relation to strain, 70
Yield point, 53
Young's modulus, 70, 73
determination uf, 74
by flexure, 99
by optical measurement, 76
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HYDROGRAPHIC SURVEYING. By Commander S.
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THEODOLITE SURVEYING. By Professor James Park.
[See page 41.
THE FORCE OF THE WIND. By Herbert Chatley, B.Sc.
[See page 23.
THE EARTH'S ATMOSPHERE. By Dr. T. L. Phipson.
[See page 46.
WIRELESS TELEGRAPHY. By Gustave Eichhorn, Ph.D.
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MINING WORKS. 39
■^A^OI^K:s sir
SIR CLEMENT LE NEVE FOSTER, D.Sc, F.R.S.
Sixth Edition. With Frontispiece and 712 Illustrations. Price 28s. net.
ORE & STONE MINING.
By Sir C. LE NEVE FOSTER, D.Sc, F.R.S.,
LATE PROFBSSOR OH MINING. ROYAL COLLEGE OF SCIENCE.
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By Prof. S. H. COX, Assoc.R.S.M.,
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INTRODUCTION. Mode of Oecuppence of Minepals.— Ppospeetlng.— Boping.
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THE INVESTIGATION OF MINE AIR:
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WORKS ON COAL-IVIINING.
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ELEMENTARY COAL-MINING;
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MINING GEOLOGY.
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Witfi Notes on tiie Valuation of Property, and Tabulating Reports,
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THE CHEMISTRY OF THE COLLOIDS.
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BLEACHING & CALICO-PRINTING.
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