Научная статья на тему 'A hydrostatic model for an ideal fluid: group properties of equations and their solutions'

A hydrostatic model for an ideal fluid: group properties of equations and their solutions Текст научной статьи по специальности «Математика»

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Ключевые слова
ИДЕАЛЬНАЯ ЖИДКОСТЬ / IDEAL FLUID / ГИДРОСТАТИЧЕСКАЯ МОДЕЛЬ / HYDROSTATIC MODEL / ГРУППОВОЙ АНАЛИЗ / GROUP ANALYSIS / ТОЧНЫЕ РЕШЕНИЯ / EXACT SOLUTIONS

Аннотация научной статьи по математике, автор научной работы — Rodionov Alexander A.

Group properties of hydrostatic model equations of a layer motion in an ideal fluid on a function defining the free surface and the thickness of the fluid layer under the free boundary are studied. Examples of several exact solutions in Cartesian and cylindrical coordinates are given, they determine the free surface and the pressure on it.

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Текст научной работы на тему «A hydrostatic model for an ideal fluid: group properties of equations and their solutions»

УДК 517.95 + 532

A Hydrostatic Model for an Ideal Fluid:

Group Properties of Equations and their Solutions

Alexander A. Rodionov*

Institute of Computational Modelling SB RAS Akademgorodok, 50/44, Krasnoyarsk, 660036

Russia

Institute of Mathematics and Computer Science Siberian Federal University Svobodny, 79, Krasnoyarsk, 660041

Russia

Received 07.01.2015, received in revised form 24.02.2015, accepted 27.05.2015 Group properties of hydrostatic model equations of a layer motion in an ideal fluid on a function defining the free surface and the thickness of the fluid layer under the free boundary are studied. Examples of several exact solutions in Cartesian and cylindrical coordinates are given, they determine the free surface and the pressure on it.

Keywords: ideal fluid, hydrostatic model, group analysis, exact solutions. DOI: 10.17516/1997-1397-2015-8-3-320-326

1. Problem statement. Basic equations

Consider equations of motion for an ideal incompressible fluid in a gravitational field

Ut + UUX + VUy + wuz + 1 px =0, Vt + UVx + VVy + WVz + ^Py = 0,

P 1 P (1)

Wt + UWx + VWy + wwz + —Pz = -g, Ux + Vy + wz = 0.

Here u, v, w are components of the velocity vector; the pressure p is the function of the variables x, y, z and of time t; the fluid density p is constant (we can take p =1); g = const > 0 is the acceleration of the force of gravity which acts in the negative direction of the z axis. Let us assume that pressure in the fluid depends linearly on the depth

Pz = -g. (2)

This assumption is often used to describe processes in oceanography [1]. Then

p(x, y, z,t) = -gz + q(x, y,t), (3)

where q(x, y, z) is a new function. In this situation the system (1) is rewritten in the following form

Ut + UUX + VUy + wUz + qx =0, Vt + uVx + VVy + wVz + qy =0,

(4)

wt + uwx + Vwy + wwz =0, ux + Vy + wz = 0.

Let z = n(x, y,t) be the equation of the free boundary on which the dynamic and kinematic conditions are fulfilled

p(x,y, n(x,y,t),t) = Pa(x,y,t); (5)

* [email protected] © Siberian Federal University. All rights reserved

nt + u(x, y, y, t), + v(x, y, y, t), t)ny = w(x, y, n(x, y, t),t), (6)

where pa(x,y,t) is the atmospheric pressure.

From formula (3) taking into consideration the condition (5) on the free surface we find that

Pa(x, y, t) = -gn(x,y,t) + q(x, y,t). (7)

Equation (7) determines uniquely the free surface via the function q(x, y, t) that can be derived from the system (4).

Sometimes it is convenient to solve the equations in cylindrical coordinates. Let us rewrite the system (4) using the variables (r, 0, z)

__ V2 _ __ V_ __ uv 1

Ut + u«r + - ug + wuz---+ qr = 0, Vt + uvr + - vg + w vz +---+ - qg = 0,

r r r r r (8)

V _ _ 1 _ _ 1 _

wt + u wr +—wg + w wz =0, ur +—vg + wz +—u = 0.

Here (U,V,w) are the components of the radial, azimuthal, and axial velocity dependent on (r, 0, z, t); the function q from formula (3) depends on (r, 0, t).

Along with equations (4) an approximate model is also considered, which describes the motion of the fluid as z ^ ez, w ^ ew. In the limit, as e ^ 0, the system (4) assumes the following form

ut + uux + vuy + wuz + qx =0, vt + uvx + vvy + wvz + qy = 0,

(9)

ux + Vy + wz = 0, qz = 0.

We perform the group analysis for systems of equations (4) and (9), find the Lie algebra of admissible operators of these systems and construct exact solutions.

2. Group properties of the equations

Study the group properties of equations (4). We introduce the following index notation u1 = u, u2 = v, u3 = w, u4 = q, x1 = x, x2 = y, x3 = z, x4 = t. In this notation equations (4), being supplemented by the requirement qz = 0, assume the following form

u4 + u1u1 + u2u2 + u3u3 + u4 = 0, u2 + u1u2 + u2u2 + u3ug + u4 = 0, u3 + u1uf + u2uf + u3u3 = 0, u1 + u2 + u3 = 0, u3 = 0.

The lower index is the differentiation.

We find an admissible operator for the system (9) in the form

d d

X = (x,u) dx + nk (x,u) duk.

Here the summation is over i, k =1, 2, 3, 4. The operator prolongs to the first derivatives

X = X + ckA ck = + ui_ uk (^+uidej

X = X + Ci duk , Ci = dxi + ui du' uH dxi + ui du' From the invariance criterion [2], acting by operator X onto equations (10), we get the

defining equations. Passing to the manifold (10) we replace u4, u4, u4, u3, u3 with the remaining variables. Splitting the defining equations with respect to the independent variables, we obtain the coordinates of the operator X

e1 = (C + C2)x1 + C3x2 + f1(x4), £2 = (C + C2)x2 - C3x1 + f2(x4),

e3 = C2X3 + C4X4 + C5, e4 = C2X4 + C6,

n1 = C1U1 + C3U2 + /1 (x4), n2 = C1U2 - C3U1 + /2(x4), n3 = C4,

n4 = 2C1U4 - x1/',(x4) - x2/2'(x4) + h(x4),

where C1;..., C6 are constant, /1(x4), /2(x4), h(x4) are arbitrary functions.

Assuming successively the constants and functions to be non-zero, we find the basis of admissible operators. In Cartesian coordinates the basis of operators for the system (4) is as follows

ddddd dddd X1 = x— + y — + u— + V— + 2q—, X2 = x — + y^- + z— + t—, dx dy du dV dq dx dy dz dt

d d d d dddd

X3 = Vt,--x— + V---u—, X4 = t— + —, X5 = —, X6 = ,

dx dy du dV dz dw dz dt , .

dd d dd d X7/1) = /1(t)dx + /1(t)— - x/1'(t)-, x8(/2) = /2(t)dy + /2(t)dV - y/2'(t)dq,

d

x9(h) = h(t) dq.

The first two operators are responsible for dilatation transformations, the third one for rotation in the plane (x; y), the fourth and fifth operators for the Galilean transformation and translation along the axis z, the sixth for translation along the t-axis. The last three operators contain three arbitrary time-dependent functions and define an infinite-dimensional part of the Lie algebra of the admissible operators.

A similar group analysis was performed for the equations with the long wave approximation in [3]. The model equations were considered in modified variables that take into account the depth of the fluid layer.

In cylindrical coordinates the operators (11) can be written down as follows

- d d d d - d d d X1 = + u—+ + 2q—, X2 = r — + z — + t —, dr du dV dq dr dz dt

X = ¿, X4 = ^ + dw-, X5 = dz, X6 = d? X9 = h(t)dq,

xx7(/1) = /1(t)cos ^ - /1(t)^l? + (-/1(t)si^-+/1(t)cos e) ddU+

+ (/1(t)""n~U - /1(t)sin ^ d- - /1'(t)r cos XX8(/2)= /2 (t) sin fld- + /2(t)C°^ | + (/2(t)C0S^ V + /2(t)sin ^ dU +

+ ( /2(t)~~~~U + /2(t)cos^ d- - /2'(t)rsin Calculations show that the Lie algebra of the approximate model (9) is

Y1 = dt, Y2 = ydx - xdy + Vd„ - udv, Y3 = -tdt + ud„ + Vdv + wd№ + 2qdq Y4 = zdz + wdw, Y5 = / (x,y,t)dz + (/xu + /y V + //)dw, Y6 = /1(t)dx + /1d„ - x/1'dq, Y7 = /2 (t)dy + /2dv - y/2'dq, Y8 = 2h(t)dt + h'(xdx + ydy - 2zdz) + (-h'u + h"x)d„ + (-h'V + h"y)d„-- (4h'w + 2h''z)dw - (Vq + hA dq, Y9 = ^(t)dq,

(12)

where f (x,y,t), f1(t), f2(t), h(t), y(t) are arbitrary functions.

In the stationary case when the functions do not depend on time the Lie algebra of admissible operators for equations (9) has the form

dx, dy, d„, zdz + wdw, ud„ + vd^ + wd№ + 2qd„, xdx + ydy - wd№,

(14)

ydx - xdy + vd„ - udv, f (x, y)dz + (fxu + fyv)d№.

3. Exact solutions

Example 1. Let us find a solution to (9) for the operators (15,17} from the basis (13) with f = f (x,t), f2 = 1. The invariants of the operators are {x,t, u,v,q, wf (x,t) - (ufx + ft')z}. Hence an invariant solution should be of the form

(u, v, w, q) = (U(x, t), V(x, t), W(x, t) + (U(x, t)fx/f + ft'/f )z, Q(x, t)).

The system of equations (9) transforms into the factor system

U' + UUx + Qx =0 V + UVx = 0 U* + f + f ="' (15)

The last equation is integrated to give

U=Tib( f dx+v(i))

f(x,t)

with an arbitrary function y(t). The functions V(x,t) and Q(x,t) are determined from the first two equations of the system (15).

Suppose that f = f(x) does not depend on time t, in which case we get the following solution of equations

(t) (t)F''(x)

u = U = -f); v = V[F(x) - -(t)]; w = ((J, )(2 ) z + W(x,t); F'(x) (F'(x))2

2 (16) q=Q = -I K) dx-KH) + ««

with arbitrary functions —(t), F(x) and f (x) = F'(x); functions V and W are arbitrary as well. From equation (7) we derive the function that defines the free boundary

n(x, y, t) = 1 (Q(x,t) - Pa (x, y, t)), (17)

g

on which the kinematic condition (6) is met

- '(t)F' '(x)

nt + U(x,t)nx + V(x,t)ny = ..V n + W(x,t). (18)

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(F (x))2

Substitute the relations (16) and (17) into (18) to obtain a condition for pa(x,y,t)

—F''

Pat + Upax + Vpa„ - (^7)2 Pa = Qt + UQx - gW. (19)

The function W(x,t) is arbitrary, this implies that we may equate the right hand side of (19) to zero. Then the equation (19) can be integrated with respect to pa to give

Pa(x, y, t) = F'(x) • P(F(x) - -(t), y - (F(x) - -(t))t)

with an arbitrary function P of two arguments.

Example 2. Let us find a solution to the system of equations (8) for the operators (X3, X4) from the basis (12). The invariants of the operators are {r, t, u, v, w — z/t, q }, so the invariant solution should be of the form

(u, v, w, q) = (U(r, t), V(r, t), + W(r, t), q(r, t)) .

The system of equations (8) transforms into the factor system

1 2 1

Ut + UUr — -V2 + qr =0, Vt + UVr + -UV = 0,

Wt + UWr + 1 W = 0, Ur + ^ + ^ U = 0. t t r

The equations (20) are integrated starting from the last equation, U = — + ^, V = 1F (A) W = !g(A)

(20)

q =|(-Ut — UUr + V) d- + ^(t) = —— y/(t) In r — ^ +/1F2(A)d- + ^(t)

(21)

where <^(t), ^(t), F(A), G(A) are arbitrary functions, A = tr2 — 2/ ty(t) dt. The kinematic condition (6) in cylindrical coordinates has the form

S + u m + — WW = 0. (22)

From equation (7) in cylindrical coordinates we find

po(r,0,t) = q(r, 0,t) — gn(r,0,t). (23)

Suppose that n = n(-,t), dn/d0 = 0. By substituting (21) into (22), we get a solution n(r,t) = tH(A) — G(A) with an arbitrary function H(A). From (23) we derive the external pressure on the free surface

3r2 ^2(t) f 1

Po(r, t) = q(r, t) — gn(r, t) = — — ¥>'(t) lnr — ^ +J ^F2(A) dr + V(t) — g(tH(A) — G(A)).

Example 3. We find the solution to equation (8) for the following two operators (Xi,X3) from the basis (12). The invariants of the operators are {z, t, u/r, v/r, w, q/r2}. The invariant solution is found in the following form

(u,V,w,q) = (rU(z,t),rV(z,t), W(z,t), —r2Q(t)) . (24)

By inserting it into equation (8), we arrive at the factor system

Ut + U2 + WUz — V2 — 2Q = 0, Vt + WVz + 2UV = 0,

(25)

Wt + WWz =0, 2U + Wz = 0.

From the third equation of the system (25) we find an implicit representation of the solution W = $(z — tW) with an arbitrary function p = z — tW. The remaining equations of the

system (25) define the functions

U = —1 Wz, V = —, Q = —1 Wzt + 1(Wz )2 — 1 WWzz — (—)2, (26)

2 Wz 4 8V ^ 4 VwJ v '

where R = R(W) is an arbitrary function. The second equation follows from the third one.

Assume that the function = + p is linear, a, p are constant. Then from (26) we see that

W

az + fi 1 + at '

U = -

a V = Ro(1 + at) Q =1

2(1 + at) ' = a ' Q =8

3a2

4R2(1 + at)2

(1 + at)2

. (27)

Here a > 0, also it is taken into consideration that the function Q depends only on t, therefore R = R0 is constant. Thus, we have the exact solution (u, v,w), q) of equations (8).

The kinematic condition (22) in cylindrical coordinates in the given situation has the following form

dn ra dn rRo(1 + at) dn az + fi dt ' =

+

2(1 + at) dr The solution to that equation is the function

<9(9

nM,t) = -fi + 1+atFÎrv/T+^t, 9 -

aa

1 + at

2rR0(1 + at)2

3a

which describes the free surface of the fluid z = n(r, 9,t). The function F depends on two arguments and is arbitrary. The external pressure on a free surface is determined by formula (23): pa (r, 9, t) = q(r, t) — gn(r, 9, t) or

Pa =

8

3a2 4R2(1 + at)2

(1 + at)2

g

fi 1 + at f n- „ 2rRo(1 + at)2 \

If a = 0 then W = p is constant. In this case the solution to equations W = p = const are the following functions

4

r 2

u = 0, v = rVo, w = P, q = "2Vo , Vo = const.

From the kinematic conditions (22) we find the function of the free surface n = pt + F(r, 0 — Vot) with an arbitrary function F, and from (23) we determine the external pressure on the free surface

4

Pa(r, 0, t) = q(r, t) — gn(r, 0, t) = y Vo2 — g(pt + F(r, 0 — Vot).

For the system of equations (25) we introduce the Lagrangian coordinates (z, t) ^ (Z, t) in such a manner that

dz

- = W (z,t), z^o = C

Denote

o o o

W = W(z(Z,t),t) = W (Z,t); V = V(z(Z,t),t) = V (Z,t); U = U(z(Z,t),t) = u (Z,t).

From the third equation of the system (25) it does follow that W (Z,t) = Wo(Z), where Wo

o

is the value of W for t = 0, then z = Wot + Z, z^ = 1 + tWg. From these calculations we see that Wz = Wq/(1 + tW^). We find that

U=

W

o . o

T-, V = (1 + tWg)vo(Z), w = Wo(Z),

2(1+ tW^ )

O o o 2 o 2 3 Wn

Q=Ut + U2— V2 = - 0

_ " 0__V 2 (Z )

4(1+ tW,5)2 V0 (Z),

2

a

2

r

2

a

a

o

where V0(Z) is the value of V(Z, t) for t = 0. Since Q = Q(t) does not depend on Z, W = a = const, V0 = R0/a = const, and

Q (t) 3a R2(1 + at)2 о Ro(1 + at) o a o Z + ( )

Q(t) = 8(T+~aty2--2a2 ' V=-a-' U= -20TO) ' W= aZ + в (28)

where a and в are constants. The solution (28) in Lagrangian coordinates coincides with the solution in Euler coordinates. The solution (28) shows that the system of equations (25) has no other solutions besides (27).

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The author is grateful to Professor V.K. Andreev for useful discussions.

References

[1] K.F.Bowden, Physical oceanography of coastal waters, Ellis Horwood Limited Publishers, New York, Halsted Press, 1983.

[2] L.V.Ovsjannikov, Group analysis of differential equations, Moscow, Nauka, 1978 (in Russian).

[3] A.A.Chesnokov, Symmetries and exact solutions of equations for shallow water of space translation flow, Zhurnal prikladnoi mehaniki i tehnicheskoi fiziki, 49(2008), no. 5, 41-54 (in Russian).

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Александр А. Родионов

Исследованы групповые свойства уравнений гидростатической модели движения слоя идеальной жидкости относительно функции, определяющей свободную поверхность и толщину слоя жидкости под свободной границей. Даны примеры нескольких точных 'решений в декартовых и цилиндрических координатах. Они определяют свободную поверхность и давление на этой поверхности.

Ключевые слова: идеальная жидкость, гидростатическая модель, групповой анализ, точные решения.

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