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DTNSRDC-82/077 


ONAL PRINCIPLE ASSOCIATED WITH A LOCALIZED NUMERICAL SOLUTION 


ADY FREE-SURFACE FLOWS 


DAVID W. TAYLOR NAVAL SHIP 
RESEARCH AND DEVELOPMENT CENTER 


Bethesda, Maryland 20084 


A VARIATIONAL PRINCIPLE ASSOCIATED WITH A 
LOCALIZED NUMERICAL SOLUTION OF UN- 
STEADY FREE-SURFACE FLOWS 


DOCUMENT 
COLLECTION 


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SHIP PERFORMANCE DEPARTMENT 
RESEARCH AND DEVELOPMENT REPORT 


September 1982 DTNSRDG-82/077 


MAJOR DTNSRDC ORGANIZATIONAL COMPONENTS 


DTNSRDC 
COMMANDER 00 
TECHNICAL DI athe hy 


OFFICER-IN-CHARGE 
CARDEROCK 


OFFICER-IN-CHARGE 


ANNAPOLIS 


SYSTEMS 
DEVELOPMENT 
DEPARTMENT 


AVIATION AND 
SURFACE EFFECTS 
DEPARTMENT 


SHIP PERFORMANCE 
DEPARTMENT 


15 


COMPUTATION, 
MATHEMATICS AND 
LOGISTICS SERA es 


STRUCTURES 


DEPARTMENT 


PROPULSION AND 


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SE Oeics AUXILIARY SYSTEMS 


eal DEPARTMENT 
19 
SHIP MATERIALS CENTRAL 
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A VARIATIONAL PRINCIPLE ASSOCIATED WITH A ae 
LOCALIZED NUMERICAL SOLUTION OF UNSTEADY are, 


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Bev Nam 


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David W. Taylor Naval Ship Research Program Element 61153N 
and Development Center Task Area RRO140302 


Bethesda, Maryland 20084 Work Unit 1542-018 


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September 1982 


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Variational Principle Numerical Ship Hydrodynamics 
Finite Element Technique Nonlinear Theory 

Free Surface Convolution 

Functional 


. ABSTRACT (Continue on reverse side if necessary and identify by block number) 

In this report, a variational principle for unsteady body wave problems 
is treated both with and without a convolution integral and with both linear 
and nonlinear free-surface conditions. Functionals are obtained for the 
numerical computation of unsteady flow fields near a body that moves on or 
beneath the free surface. This formulation can be applied to ship hydro- 
dynamic performance problems of water entry and body slamming, as well as to 
arbitrary body motion. 


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TABLE OF CONTENTS 

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NOTATION 


D Fluid domain 

f; Function defined in Equation (23) 
g Acceleration of gravity 

By Function defined in Equation (24) 
h Body or free surface defined in Equation @)) 
J Functional 

m Source distribution 

Pp Pressure distribution 

Sp Free surface 

Sy Interface of near and far fields 
S. Body surface 

t Time 

Viet Rectangular Cartesian coordinates 
0) Variation 

0 Water density 

T Time 

a) Potential 

w Function defined in Equation (21) 
w Frequency defined in Equation (21) 
Subscript 

i The ith order 

n Normal derivative toward fluid 

fe) Projection on the z = 0 surface 

t The time derivative 


iv 


The z derivative 
Near field, the first order 


Far field, the second order 


ABSTRACT 


In this report, a variational principle for unsteady body 
wave problems is treated both with and without a convolution 
integral, and with both linear and nonlinear free surface con- 
ditions. Functionals are obtained for the numerical computation 
of unsteady flow fields near a body that moves on or beneath the 
free surface. This formulation can be applied to ship hydro- 
dynamic performance problems of water entry and body slamming, 
as well as to arbitrary body motion. 


ADMINISTRATIVE INFORMATION 
The work reported herein has been supported by the Numerical Naval Hydrodynamics 
Program at the David W. Taylor Naval Ship Research and Development Center. This 


program is jointly sponsored by the Office of Naval Research and DINSRDC under Task 
Area RRO140302, Work Unit 1542-018. 


INTRODUCTION 

In the early 1970's the David W. Taylor Naval Ship Research and Development 
Center (DTNSRDC) recognized the demand for advanced numerical methods to predict the 
hydrodynamic performance characteristics of naval ships, particularly when classical 
methods proved inadequate. 

Thus, in 1974 the Numerical Naval Ship Hydrodynamics Program was begun at 
DTNSRDC. Under this program the author previously investigated the steady ship-—wave 
problem using a variational principle associated with a localized finite-element 
Pochndaeee This method is useful particularly to analyze the flow field near the 
ship in detail; in the far field, the Michell approximation can be used. This report 
extends the problem to the unsteady case. 

For both the steady and unsteady problems, the simple calculation is for a 
linear free surface condition with exact body boundary conditions. An iterative 
method is needed for a nonlinear free surface condition. However, in the unsteady 
problem, the variational principle requires an integration with respect to time using 
the initial conditions; in this instance, a convolution integral is useful. The 
variational principle for the unsteady body wave problem with exact body boundary 


conditions is treated both with and without convolution, and with both linear and 


*A complete listing of references is given on page 13. 


ai 


nonlinear free surface conditions. For the linear free surface problem, a func- 
tional for the variational principle is obtained with a convolution rather than a 
general integral. The convolution cannot be applied to a nonlinear free surface 
problem; the condition is required for large values of time. A nonlinear solution 
derived using an iteration scheme having the linear convolution form is also dis- 
cussed. The time integration can be eliminated if the motion is sinusoidal. 

This formulation can be applied to problems of water entry and body slamming, 


as well as to arbitrary body motion. 


NONLINEAR PROBLEM 
Since problems dealt with here can be generalized easily to three-dimensions, 
for simplicity we first consider a two-dimensional problem in the rectangular Car- 
tesian (x,z) coordinate* plane. When a body whose surface is represented by 


S. [z=h(x,t)] | @) 


enters the water surface Sa (Ze= 10), bes a = h(x,t), t > 0) at time t = O, or when 
a semisubmerged or fully submerged body starts to move at time t = O and either exits 
the water or stops moving at t = th» then the boundary conditions for a velocity 


potential $¢ are as follows: 


¢ = >, = 0 for t < 0 everywhere 


+ (1b)? - 6, + gh=0 oS (2) 


h - VoV (h-z) = 0 
h_ - ® eo = 0 
t n x 


Here, S(t) is the submerged body surface varying with time t, and n is the normal 


direction into the fluid. We consider potentials 1 in the domain Dy and >, in the 


*Definition of notations are given on page iv. 


domain Dos where dD, is the near field including 85> and Dy is outside of D,- Then 
at the interface Sy of D, and Das we need to have 


(4) 
¢,--¢ 


n 2n 
The outer potential 5 in Ds is assumed to satisfy the linear free surface condition 


ate t SPon © o 


For such 5 we know the time-dependent Green fundetor 


Now we will construct a Lagrangian for the previously described problem, con- 


sidering the Lagrangian that feateee used 


ic 


‘ 2 
1 re x 
i -| \j (5 Ma % 1-41, ) azexet +f | g > dxdt a | (0,- 5 by) bo. dzdt (6) 


a 
0 Dd, 0 Sip 0 Sy 


where P> %, and h vary with time, and t is a sufficiently large time after the body 
has either exited from or come to rest in the water so that we can safely assume that 
the variation bo), Sb, aue 5b, vanishes at t = tT. It will be shown later that the 
use of a convolution integral necessitates only the initial condition without the 
Condition at t = T. 


Since 


hiGcat ye ~niGc, t) 
ma bdz = ods + $(z=h) a (7) 


we have 


re h(x,t) h(x,t) 


{ fx] >. dzdt I aE al odz — o(z=h) hy dxdt 
0 


heat) T AE 
“| ee | | dt (z=h) he dx 
0 
or 
Ag cr 5 
{| ), dzdxdt = S| | h, ¢dxdt +f bdxdz (8) 
Dis Ce) Q ss. D, (t=t) 


Now we take a variation of J in Equation (6), and use the Green theorem, and the 


He eye aL 
condition at large t = T obtaining 


T 
1 
6J -{ | € Vo, Vy ,t2h ) Oh dxdt 


0 Sie 


au 40 
“| il vo, 89, dzdxdt I { (19/65 *,) 6h, dxdt 
0 0 3, ,Us. 


Di 1F 


i ic 
=| | (>, +45,) 66, dade = | (¢,-$5) 665, dadt 


0 Ss; 0 Sy 


i 
1 
+ “| J (50. P5409 56, ) dzdt = 0 (9) 
0 Ss 


However trom the identity, 


ff (9° 865-50" (66,)} ards -| {$, 66,-$5(8b,,)} ds = 0 
S 


7) Sor 


and from the linear free surface condition on Sop Equation (5), and the condition 


at t = T, we have 


€ i 
| J (9 55,,-$5565,) dadt = =| A (8$505,-¢5505,,) dxdt 
0 Sj 0 Se 
(10) 
iG 
. Al SUT he STP ores a | (8$.565,7$95¢5,) = dx = 0 
ope w Sop 


so that the last integral of Equation (9) vanishes. Since 5by5 5b, Sbo0> and 6h 

are arbitrary, we obtain from Equations (9) and (10) the corresponding time- 
dependent, free surface boundary value problem represented by Equations (2)-(4) 
together with the Laplace equation for ¢. Therefore, solving the variational problem 
with the functional J of Equation (6) is equivalent to solving the Laplace equation 
with the boundary conditions as set forth in Equations (2)-(4), provided we assume 


that 


6b, = 5b, = Ob, = 0 at t=T 


LINEAR PROBLEM 
If we assume a linear free surface condition in both Sip and Sop and keep the 


exact boundary condition [Equation (3)] on the body surface, 


Paper ie! nH ad 


then we may use 


18 
a {fa Vo,V$, dzdxdt - ak [ $191 ep dxdt 
OD 


iL 


{Jom f] 


where S is the projection of S, on z= 0. When we take the variation of J, we have 


Fo 
S13 AD. 
Sace Veoh edule dsdese Oe ee deat 
me Tele eee pa | UA aes, lee) oe 
anny SN 


1 
(i> 2&2) $,,dsdt (12) 


ie 
( o,, ve -,) dxdt 


T c 
-| j ($4 -%5) bo) dzdt -| j (6) 5,257 dzdt (12a) 


0 Sy 0 Sy 


Here, in addition to Equation (10), the following equation holds 


J js Care dxdt -f J Tee dxdt f i ee dxdt 


als 


Z 2) a +f 9750 OO ter OX 2 
0 “Ss 0 


Fo ene ae (13) 


Thus, as in the previous section, we can easily derive the corresponding linear free 
surface boundary value problem using Equation (5) with the exact body boundary con- 


dition in Equation (11). 


USE OF CONVOLUTION 
Equations (6) and (12) are Lagrangians in a time-dependent, two-dimensional 

space with nonlinear and linear free surface conditions, respectively. They could 

be localized in space but not in time. Namely, we had to specify the conditions on 
Se at t = 0 and t = Tt with a sufficiently large T. On the other hand, we did not 
require the initial condition un = 0 at t = 0. In addition, such time T when 1 = 0 
on Sp may be too fleeces for practical use. For linear free surface boundary condi- 
tions, we can treat our variational problem in the same way as those who have treated 


variation principles for linear initial value problems using convolutions defined 


by 
i 
* = oe 
oT 5 :{ >, (x,z,t) (85257 t) dt 
0 
(14) 
ab ad ao ao 
= 1 2 1 D 
15 * VO5 ~ Ox z ox us Oz ; Oz 
We change Equation (12) to 
Ta ye. eo deol] Caren ecee 
2 al 1 22 il det 
an SG 
5 ak ; 
| he x %) dx | (0° 7 +, * Pon dz (GLE) 
ne Si 


If we use the identity relation 


and the initial condition %) =o = 0 at t = 0, instead of the conditions Ot = 0 on 


lt 


Sp at t = 0 and t = Tt with large T used in the previous section, we obtain, for any 


time, T 


T 1G 

s| 1 * ee dx -| 5o, (x, t) Prep Hott) dxdt | | >, (x,t) 5b pp He T-t)dxdt 
0s 0s 

Fo Fo Fo 


T 
= 2 ( 6, (x,t) dy pp So Tot dxdt 
05 
Fo 


+f {($, (x,t) S$, , (x, t-1)-$,, (x, t) 84, (x, t-t)} 14 dx 
S 
Fo 


il 
ho 
o> 


T 
| dp, (x,t) by pp Ho Tt) dxdt 
S 


Fo 


(16) 


HI 
N 
n> 
OQ 
a 
ke 
> 
rR 
ct 
Gr 
a. 
* 


where T need not be large, and x represents a point on the free surface z = 0. Thus, 


we obtain as in Equation (12a) 


2 x : 
D 
i 


Sao 


f2. 
- | 6b, * (1, hy+1 - hy] dx 


S 
Ss 

|| (5-95) * 86, dz - i (b, 45.) * 60,42 (17) 
eT aT 


To obtain Equation (17), we used a convolution expression of Equation (16), where we 


can use the initial condition 4 = =1 0; 


Ve 

Since Soy > Soo, and Soo, are arbitrary, we obtain the corresponding equations 
for a time-dependent linear free surface boundary value problem that has a unique 
solution. 


If we lift out Sy so that D, occupies the entire fluid domain, then the last 


integral of Equation (15) ieee The resulting equation appears much simpler 
than that obtained by Mapeae! due to a simple difference in the treatment of the 
free surface condition. Equation (15) does not give the wave height as a natural 
boundary condition, whereas Murray's corresponding equation does. However, from h = 
$,/8 the wave height can be obtained. 

If we consider eigen solutions that satisfy only the Laplace equation; the 
linear free surface condition, Equation (5); and the radiation condition in dD, U Dy» 


then >, which satisfies the body boundary condition in Equation (11), can be derived 


from Equations (15) and (17) by using 


1 Vid. 
= —_— — * 
J | (3 Oe hyt1 ny] odx (18) 
s 
s 
When we know a functional whose minimum value is attained by the solution, we 
can find the solution numerically by such methods as the finite-element eechatiques 
F P 9 
or singularity method. 


For example 
b= D7 a9) (19) 


where o, is the Green function, which is available for this problem for a source 
distribution on the body surface. The source distribution m; will be obtained from 


soltuion of the simultaneous equations, 


SO . fa1'2,°.2N (20) 


SINUSOIDAL MOTION 


If we consider a sinusoidal ship oscillation such as h =f Bawe for S, of 
Equation (1), we substitute 
i iwt 
into Equation (12), integrate with respect to t, and obtain 
-iwt Al, Ne 2. 
e J= Jy = > Vb, dzdx - oe vy dx 
Si Sp 
+) fb, dx-] (vw -tu,)u, 4 (22) 
i ices ( P22 5) Dass © ji 


This is exactly the same Lagrangian that Bai and Yeung. used. Working from Equation 


(18), we can apply eigen solutions to the whole field by using 


i =| (5 ¥,-F) ds 


where 
h,/ vno+1 ape 


A similar functional was used by Sao et Fale? to solve the problem of a heaving 


oscillation of a dock. 


ITERATIVE SCHEME 
For problems with the linear free surface condition, we can completely localize 
the numerical scheme in DS with 0 < t < Tt for any T with the help of the convolution 
form. However, for nonlinear problems, the finite-element technique has to rely on 


: P “ : saa oe 
an iteration. We may thus use an iterative free surface condition on z = 0 


10 


OVS gel f=: 0 (23) 
gh, - bat +g, = 0 (24) 


where, for the first order perturbation solution, fy = 0, 8) = QO and, for the nth 


order, ae and g, are known functions of 5 of the (n-1)th or the lower order 


solutions. 


Then the Lagrangian for each f. is 


1 i 
= —- * —_—— 
oe {J Paes eae | oie uae & 
Dy (z=0)ND, 
ae * * 
| $,, *f, det fo, 4, ax 
(z=0)9D, 


oa 
oJ, = 0 (25) 
where the solutions for 1= 1, 2,...n - 1 should be used to determine the solution 


when i = n. Equation (24) gives the wave height h for each i. 
If we specify a time-dependent, free surface pressure distribution p on the 


projection oan of S, to z = O instead of hy in S. we may use 


£, = 8) — p/P OD ee 


in Equations (23) and (24) for the first order, where p is the water density. 


lel! 


Although we have discussed the two-dimensional time-dependent problem, Equations 


(19) through (24) can be extended to the three-dimensional time-dependent problem. 


| al il 
= = *k Sek 
D 


That is 


l (2=0)ND, 
- \| , * fs dxdy (fr, * 4 dxdy 
(z=0)ND, 
alt 
-{{ (¢)- 2 b,)* 6, de 
=F 


and soon. 


CONCLUDING REMARKS 

We have formed functionals with both linear and nonlinear free surface boundary 
conditions. For the former but not the latter case, we could apply a convolution 
integral. However, the body boundary condition is satisfied exactly in both cases. 
In many cases, the flow field near an arbitrary body is of interest, and eigen solu- 
tions with linear free surface conditions are known. Even in any large unsteady 
motion such as ship slamming, the free surface condition for a short period in the 
beginning may be linear, then the convolution may be applied in the early time 
period. Especially in the slamming problem, the peak pressure is known to be reached 
early in the beginning and estimation of the early pressure distribution on the 
slamming body is required. With this functional, we can find the solution for an 
arbitrary body numerically by such methods as the finite element technique or singu- 


larity method. Thus, a wide application of such functionals can be expected. 


12 


REFERENCES 
1. Yim, B., "A Variational Principle Associated with a Localized Finite- 
Element Technique for Steady Ship-Wave and Cavity Problems," Proceedings of the First 
International Conference on Numerical Ship Hydrodynamics, David Taylor Naval Ship 


R&D Center (1976). 


2. Wehausen, J.V. and E.V. Laitone, "Surface Waves," Encyclopedia of Physics, 


Springer-Verlag, Berlin, Vol. IX, pp. 446-778 (1960). 


3. Stoker, J.J., "Water Waves," Interscience Publishers, Inc., New York (1957), 
pp. 187-196. 


4, Yim, B., "Investigation of Gravity and Ventilation Effects in Water Entry 
of Thin Foils," Proceedings of the International Union of Theoretical and Applied 
Mechanics Symposium held in Leningrad (1971), NAUK Publishing House, Moscow, pp. 
471-475 (1973). 


5. Luke, J.C., "A Variational Principle for a Fluid with a Free Surface," 


Journal of Fluid Mechanics, Vol. 27, Part 2, pp. 395-397 (1967). 


6. Gurtin, M.E., "Variational Principles for Linear Initial-Value Problems," 


Quarterly Journal of Applied Mathematics, Vol. 22, pp. 252-256 (1964). 


7. Murray, J.C., "A Note on Some Variational Principles for a Class of Linear 
Initial-Boundary Value Problems," Journal of the Institute of Mathematics and 


Applications, Vol. 12, pp. 119-123 (1973). 


8. Bai, K.J. and R. Yeung, "Numerical Solutions of Free-Surface Flow Problems," 


10th Symposium on Naval Hydrodynamics, Office of Naval Research (1974). 


9. Sao, K. et al., "On the Heaving Oscillation of a Circular Dock," Journal of 


the Society of Naval Architects of Japan, Vol. 130, pp. 121—=13F~ GVA”: 


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SNAME/Tech Lib 
Bethlehem Steel/Sparrows Point 
Bethlehem Steel/New York/Lib 
Exxon, NY/Design Div, Tank Dept 
General Dynamics, EB/Boatwright 
Gibbs & Cox/Tech Info 


Hydronautics/Lib 


Lockheed, Sunnyvale 
1 Potash 


Copies 
iL Newport News Shipbuilding/Lib 
at Oceanics 
il Sperry Rand/Tech Lib 


1 Sun Shipbuilding/Chief Naval Arch 


2 American Bureau of Shipping 
i Lib 
1 Cheng 

it Maritime Research Informaticn 
Service 


CENTER DISTRIBUTION 


Copies Code Name 


ili 012 D. Jewell 


Al 1170 R.M. Stevens 
ali 1170 G.R. Lamb 


i 1170 S. Hawkins 

al 1500 W.B. Morgan 

Al 1504 V.J. Monacella 
1 1520 WG. ian: 

1 1521 W.G. Day 

1 isk A.M. Reed 

ik: 522. G.F. Dobay 

al 11522 M.B. Wilson 

ih 1540 J.H. McCarthy 
ANS) 1540 B. Yim 

i 1542 T.T. Huang 

Al 1542 J. Bai 

i 1560 D. Cieslowski 
iL 1560 Division Head 
1 1561 GAG Cox 

1 1561 S.L. Bales 

1 1562 D.D. Moran 

il 1562 Es. Zarniek 
il 1562 Y.S. Hong 


16 


Copies 
aL 
AL 
1 


10 


Code 
1563 
1564 
1564 
Byala Db 
522.1 
D226 2 


Name 

W.E. Smith 

J.P. Feldman 

R.M. Curphey 

Reports Distribution 
Library (C) 

Library (A) 


Ny 


DTNSRDC ISSUES THREE TYPES OF REPORTS 


1. DTNSRDC REPORTS, A FORMAL SERIES, CONTAIN INFORMATION OF PERMANENT TECH- 
NICAL VALUE. THEY CARRY A CONSECUTIVE NUMERICAL IDENTIFICATION REGARDLESS OF 
THEIR CLASSIFICATION OR THE ORIGINATING DEPARTMENT. 


2. DEPARTMENTAL REPORTS, A SEMIFORMAL SERIES, CONTAIN INFORMATION OF A PRELIM- 
INARY, TEMPORARY, OR PROPRIETARY NATURE OR OF LIMITED INTEREST OR SIGNIFICANCE. 
THEY CARRY A DEPARTMENTAL ALPHANUMERICAL !DENTIFICATION. 


3. TECHNICAL MEMURANDA, AN INFORMAL SERIES, CONTAIN TECHNICAL DOCUMENTATION 
OF LIMITED USE AND INTEREST. THEY ARE PRIMARILY WORKING PAPERS INTENDED FOR IN- 
TERNAL USE. THEY CARRY AN IDENTIFYING NUMBER WHICH INDICATES THEIR TYPE AND THE 
NUMERICAL CODE OF THE ORIGINATING DEPARTMENT. ANY DISTRIBUTION OUTSIDE DTNSRDC 
MUST BE APPROVED BY THE HEAD OF THE ORIGINATING DEPARTMENT ON A CASE-BY-CASE 
BASIS.