______________________________________
* Corresponding Author: [email protected] (M. S. Parvin)
App. Math. and Comp. Intel., Vol. 3 (1) (2014) 259–272 http://amci.unimap.edu.my
© 2014 Institute of Engineering Mathematics, UniMAP
Mass Transport Velocity in a Two-dimensional Wave Tank
M. S. Parvina*, M. S. Alam Sarkera, and M. S. Sultanaa
aDepartment of Applied Mathematics, University of Rajshahi, Rajshahi-6205, Bangladesh
Received: 13 July 2013; Accepted: 23 November 2013
Abstract: Waves occurred on the surface of water in two-dimensional wave tank are studied.
Deriving vorticity equation from incompressible Navier-Stokes equation, the boundary condition on the free surface, water bottom and flap surface are discussed. Using separation of variable method, velocity potential takes the general form in terms of eigen function. To obtain the values of horizontal and vertical velocity components, the boundary conditions on the water bottom and the flap surface are used and then mass transport velocity has been derived. Finally, time average of horizontal velocity component at mean water level is generalized.
Keywords: Mass Transport Velocity, Navier-Stokes Equation, Stream Function.
1. Introduction
A basic theory for the mass transport velocity in water waves in viscous fluid and of finite depth has been formulated. Longuet-Higgins [1, 2, 3] presented a simple physical model to obtain the Lagrangian characters including particle motion, mass transport, the Lagrangian wave period and the Lagrangian mean level for the surface waves that cannot directly obtain throughout the entire flow field. Hsien- Kuo et al. [4] discussed gravity waves in water of uniform depth of governing equation in Lagrangian form. If a small neutrally buoyant float is placed in a wave tank and its trajectory was traced as waves pass by, a small mean motion in the direction of the waves can be observed. There are two approaches for examining the mass transport, one is the Eulerian velocity which involves a fixed point to measure the mean flux of mass and other is the Lagrangian velocity which involves moving with water particles. The stream function for mass transport is calculated from the products of the first order eigen functions for progressive and local waves. Naciri and Mei
260 M.S. Parvin et al.
[5] also constructed Lagrangian asymptotic solutions of the non-linear water waves. Iskandarani and Liu [6] discussed on mass transport in two-dimensional wave tank. Many Lagrangian asymptotic solutions of the non-linear water waves have been developed such as Buldakov et al [7], Clamond [8] and Constantin [9]. Boufermel et al. [10] formulated velocity of mass transport taking as variable to model acoustic streaming. Frode [11] studied mass transport velocity in shallow water waves reflected at right angles from an infinite and straight coast in a rotating ocean. In this paper, mass transport velocity has been formulated using boundary conditions at water bottom and the flap surface. Finally, we see that the time average of horizontal velocity component is zero at mean water level which is same as Dean and Dalrymple [12].
2. Mathematical Formulation 2.1. Governing Equation
The motion of the water surface consists in general regular waves for local disturbance progressing on a constant water depth
( z = h )
as shown in Fig.1.Figure1: Wave Train
Mass transport velocity (
ε
2U
1, ε
2W
1), defined as the average of the Lagrangian velocity which is in terms of particle velocity and stream function can be written as2
.
1 2 1 1
2 1 1
1
dt z z
x z
dt x u z
U ∂
Ψ
= ∂
∂
∂
∂
− ∂
∂
∂
∂
∂ + ∂
= ∫ ψ ψ ∫ ψ ψ
(1) andWaves
h z
x
App. Math. and Comp. Intel., Vol. 3 (1), 2014 261
1
.
2 1 2
1 2 1 1
1
dt x z x
x x z dt w
W ∂
Ψ
− ∂
∂ =
∂
∂
∂ + ∂
∂
∂
∂
− ∂
= ∫ ψ ψ ∫ ψ ψ
(2)For the mass transport velocity
U
, the stream functionΨ
can be written as1
.
1 2
+ ∫ ∂ ∂ ∂ ∂
=
Ψ dt x
z ψ
ψ ψ
(3)The Navier-Stokes equation for incompressible flow is
1
2.
u F
p z u
x w
t u = − ∇ + + ∇
∂ + ∂
∂ + ∂
∂
∂ υ
ρ
(4) Whereu and w
denote the horizontal and vertical velocity components respectively,p
is the pressure gradient,F
is the external body force andυ
denotes the kinematic coefficient of viscosity where,ρ υ = µ
.Taking curl on both sides of Eq. (4), we have
ξ υ ξ = ∇
2
∂ + ∂
∂ + ∂
∂
∂
w z u x
t
, since, vorticityξ = ∇ × u
(5)( )
=
+
−
∇
×
∇
∇
−
=
−
= , φ 0
φ ρ ρ
ρ g and p
F
QNow, the vorticity equation from the above equation is in the following
.
2
0
2
∇ =
− ∇
∂ + ∂
∂ + ∂
∂
∂ υ ψ
w z u x
t
(6)where,
∂
− ∂
∂
− ∂
∂
∂
∂
= ∂
∂
∂
∂
− ∂
∂
∂
∂
= ∂
∂
− ∂
∂
= ∂
×
∇
= z x z z x x x z z
u x
u w φ φ ψ ψ
ξ
2
.
2 2 2 2
ψ ψ = ∇
∂ + ∂
∂
= ∂
z x
Now,
1
.
4 1
2
= ∫ ∇
∇ ψ υ ψ dt
(7) [taking first-order term of Eq. (6)]and
2
.
4 1 2 1
1
∇ ψ = υ ∇ ψ
∂ + ∂
∂
∂ w z
u x
(8)262 M.S. Parvin et al.
[taking time average of second-order term of Eq. (6)]
Using Eq. (7) in Eq. (8), we have
1
.
4 1
1 2
4
dt
w z
u x ∫ ∇
∂ + ∂
∂
= ∂
∇ ψ ψ
(9)From Eq. (3), the stream function for the mass transport velocity
U
can be written as1
.
4 1 1 4 1
1
4
Ψ = ∂ ∂ + ∂ ∂ ∫ ∇ + ∇ ∫ ∂ ∂ ∂ ∂
∇ dt x
dt z w z
u x ψ ψ
ψ
(10) Assumingψ
1 satisfies Laplace equation, Eq. (10) which is considered as the boundary layer theory can be rewritten as1
.
4 1
4
Ψ = ∇ ∫ ∂ ∂ ∂ ∂
∇ dt x
z ψ
ψ
(11)According to Longuet-Higgins [1], boundary condition for
Ψ
on the bottom of water is given by( ) ( )
.
4 3
5
*1 1
∞
∞
∞
=
∂
∂
= −
∂ Ψ
∂
s s n
s q i q
i
n ω
(12) whereq
s( )∞1 represents the first order tangential velocity at outer edge of the boundary layer at the fixed wall and superscript * represents the complex conjugate of the value and the boundary condition at free surface is( ) ( )
.
4
0*1 0 2 1
2
s n n
s q s q i
n ∂
∂
∂
= ∂
∂ Ψ
∂
∞
=
ω
(13) 2.2. Linear Water Wave TheoryLinear water waves are of small amplitude for which we can linearise the equations of motion. The water wave motion is represented by a velocity potential
Φ ( x , z , t )
which is considered as( x , z , t ) = Re { φ ( x , z ) e
iωt} .
Φ
(14) We assume that the bottom surface is of constant depth atz = − h
.The water surface is at= 0
z
and the region of interest is− h < z < 0
. Now the equations are in the following= 0 +
zzxx
φ
φ
,− h < z < 0 .
(15)
=
∂ =
∂
−
=
∂ =
∂
. 0 ,
, ,
0
z z K
h z z
φ φ φ
(16)
App. Math. and Comp. Intel., Vol. 3 (1), 2014 263
The last expression can be obtained from combining of the following two equations
=
=
=
±
∂ =
∂
. 0 ,
, 0 ,
z g i
z z i
η ωφ φ ωη
m(17)
where
...
,...
2 , 1 , tan tanh
2
=
−
=
=
=
n h k k
kh g k
K
n n
ω
(18)
Eq. (15) is solved by the separation of variable method. So the velocity potential
φ
are taken as( x , z ) = U ( ) ( ) x P z .
φ
(19) Substituting this value in Eq. (15), we have1 . 1
2 2 2
2
dz P d dx P
U d
U = −
(20) The L.H.S of Eq. (20) is only a function ofx
and the R.H.S of Eq. (20) is only a function ofz
. So each term is constant. Therefore,1 .
1
22 2 2
2
dz k P d P dx
U d
U = − = ±
(say) (21) Taking positive sign, we have from Eq. (21),.
2
0
2 2
= + k P dz
P
d
(22)and
.
2
0
2 2
=
− k U dz
U
d
(23)Solving Eq. (22), we obtain
( ) z Ae
ikzBe
ikzP = +
− , where A and B are arbitrary constants. Therefore, Eq. (19) becomes( x , z ) = ( Ae
ikz+ Be
−ikz) U ( ) x .
φ
(24) Applying boundary condition| = 0
∂
∂
=h
z
zφ
in Eq. (24), we getA = Be
−2ikh.
Hence,
( ) z D cos k ( z h ) .
P = −
=
= Be
−ikhD 2
constant.Therefore, Eq. (24) becomes
264 M.S. Parvin et al.
( x , z ) = D cos k ( z − h ) ( ) U x .
φ
(25) Again, solving Eq. (23), we havekx
kx
B e
e A
U =
1+
1 − , whereA
1and B
1 are arbitrary constants.If we set
A
1= 0 and B
1= 1
, thenU = e
−kx.
Therefore, Eq. (25) becomes( x , z ) = D cos k ( z − h ) e
−kx.
φ
(26) Using Eq. (17) in Eq. (26), we have0 ,
sin = − =
−
∂ =
∂
−z i khe
z Dk
kx
ωη
φ
. 0 ,
sin = =
⇒ Dk khe
−kxi ωη z
(27) This expression forφ and η
become more convenient if we writeη = ae
−kx, Eq. (27) can be written assin kh . k D ai ω
=
Substituting the value of
D
in Eqs. (24) and (26), we have( ) cos ( ) .
, sin k z h e
kxkh k z ai
x = ω −
−φ
(28) and( ) cos ( ).
sin k z h
kh k z ai
P = ω −
(29) The boundary condition at the free surface gives
ω
2= − gk tan kh
, which is the dispersion relation for a free surface.The above equation is not really the dispersion relation for a free surface, it would be better to refer to it as a transcendental equation. If we solve for all roots in the complex plane, we find that the first root is a pair of imaginary roots. We denote the imaginary solutions of this equation by
ik
k
0= ±
and real solution byk
n, n ≥ 1
. Thek
of the imaginary solution is the wave number.So we put
ω
2= gk tanh kh
.Finally, we define the function
P ( ) z
as( ) cos ( ), 0 .
sin − ≥
= k z h n
h k k
i z a
P
nn n
n
ω
App. Math. and Comp. Intel., Vol. 3 (1), 2014 265
as the vertical eigen function in the open water region.
Also, we can write
U = e
−knx.
Hence, the velocity potential eigen function expansion can be written as
( ) cos ( ) .
, sin
n k xn n
n
k z h e
nh k k
i z a
x = ω −
−φ
(30) Using Eqs. (18) in (30), we have( ) cos ( ) .
, cos
n k xn
n
k z h e
nh k K
i z a
x = − ω −
−φ
(31)Similarly, taking negative sign, we have from Eq. (20),
.
2
0
2 2
=
− k P dz
P
d
(32)and
.
2
0
2 2
= + k U dz
U
d
(33)Solving Eq. (32), we have
( ) z A e
kzB e
kzP =
2+
2 − , whereA
2and B
2 are arbitrary constants. Therefore, Eq. (18) becomes( x , z ) = ( A
2e
kz+ B
2e
−kz) U ( ) x .
φ
(34) Applying boundary condition| = 0
∂
∂
=h
z
zφ
in Eq. (34), we getA
2= B
2e
−2kh.
Hence,
( z h )
k D
P =
1cosh −
, where,D
1= 2 B
2e
−kh=
constant.Therefore, Eq. (34) becomes
( x , z ) = D
1cosh k ( z − h ) ( ) U x .
φ
(35) Again, solving Eq. (33), we haveikx
ikx
B e
e A
U =
3+
3 − , whereA
3and B
3 are arbitrary constants.If we set
A
3= 0 and B
3= 1
, thenU = e
−ikx.
Therefore, Eq. (35) becomes( , )
1cosh ( ) .
e
ikxh z k D z
x = −
−φ
(36) Using Eq. (17) in Eq. (36), we have266 M.S. Parvin et al.
. 0 ,
1
sinh = =
∂ =
∂
−z i khe k
z D
ikx
ωη
φ
. 0 ,
1
sinh = =
⇒ D k khe
−ikxi ωη z
This expression for
φ and η
become more convenient if we writeη = ia
0e
−ikx, we getsinh .
0
1
k kh
D a ω
−
=
Hence, from Eq. (36), we have
( ) cosh ( ) .
, sinh
0k z h e
ikxkh k
z a
x = − ω −
−φ
(37) Using Eq. (18) in Eq. (37), we have( ) cosh ( ) .
, cosh
0k z h e
ikxkh K
z a
x = − ω −
−φ
Therefore,
( ) ( ) cos ( ) .
cosh cos , cosh
1
0
∑
∞=
−
−
− −
−
−
=
n
x k n
n n
ikx
k z h e
nh k K
i e a
h z kh k
K z a
x ω ω
φ
[Using eigen function expansion]
In general form, the velocity potential can be expressed as
( ) ( )
( )( )
− − − −
=
Φ ∑
∞=
−
−
−
1
0
cos
cosh cos Re cosh
, ,
n
t i x k n
n n t
kx
i
k z h e e
h k K
i e a
h z kh k
K t a
z
x ω
ωω
n ω( ) ( )
( )( )
− − + −
=
⇒ Φ ∑
∞=
−
−
−
1
0
cos
cosh cos Re cosh
, ,
n
t x i k n
n n
n t
kx
i
k z h e e
h k k
i e a
h z kh k
k t a
z
x ω
ωω
n ω[Qfrom Eq. (18),
K = k = − k
n ]( ) ( )
( )( )
− + −
=
Φ ∑
∞=
−
−
−
1 2 0
cos cos cosh cosh
Re , ,
n
t i x k n
n n t n
kx
i
k z h e e
h k k
i e a
h z kh k
k i a t
z
x ω
ωω
n ω( ) ( )
( )cos ( ) .
cosh cos Re cosh
, ,
1 0 0
2 0
− + −
=
⇒ Φ ∑
∞=
−
−
−
n
t i x k n
n n t n
kx
i
k z h e e
h k k
K i e a
h z kh k
k K i a
t z
x θ ω
ωθ ω
n ω[Assuming
K
1
0
=
θ
]App. Math. and Comp. Intel., Vol. 3 (1), 2014 267
( , , ) Re { 0 1( , ) } .
t
e
iz x i
t z
x = ωθ φ
ωΦ
∴
(38) where,( ) ( ) cos ( ) .
cosh cos , cosh
1 0
1
∑
∞=
−
+ −
−−
=
n
x k n
n n
ikx n n
e h z h k
k k e Ka
h z kh k
k i z Ka
φ x
(39)2.3. Formulation of mass transport velocity
The first order potential
φ
1( x, z )
can be written by the eigen function expansion,( ) ( ) ( )
k xn n n n
n
ikx
e
nh k
h z k k a K kh e
h z k k ia K z
x
−∞
=
−
−
− +
= ∑
cos cos cosh
, cosh
1 0
φ
1 , [From Eq. (39)]( )( ) ( )
cos . sin cos
cosh cos cosh
1 0
x k n n n n
n
e
nh k
h z k k a K kx
i kh kx
h z k k
ia K
−∞
=
+ −
− −
= ∑
(40)Substituting this value in Eq. (38), we get
( )
( ) ( )
( )
+ −
− −
= Φ
∞ −
=
∑
t i x
k n
n n n
n
e h e
k h z k k a K
kx i kh kx
h z k k
ia K
i t
z x
n
ωθ
ωcos cos
sin cosh cos
cosh Re
, ,
1 0 0
( )( )
( ) ( )
+
+ −
− −
−
=
∞ −
=
∑ e t i t
h k
h z k k a K i
kx i kh kx
h z k k a K
x k n n n n
n
n
ω ω
ωθ cos sin
cos cos
sin cosh cos
cosh Re
1 0 0
( ) ( { ) ( ) }
( ) ( )
− − + −
− +
− +
−
=
−
∞
=
−
∞
=
∑
∑ e t
h k
h z k k a K t h e
k h z k k a K i
t kx t
kx i t kx t
kh kx h z k k a K
x k n n n n
n x
k n n n n
n
n
n
ω ω
ω ω
ω ω
ωθ
cos sin cos cos
cos cos
cos sin sin
cos sin
sin cos
cosh cos cosh Re
1 1
0 0
( ) ( ) ( )
( ) ( ) ( )
. cosh sin
cos cosh cos
cos
cos sin cos cos
cosh cosh Re
0 1
1 0
0
− −
− − +
− −
− −
−
=
−
∞
=
−
∞
=
∑
∑
t kh kx
h z k k a K t h e
k h z k k a K i
t h e
k h z k k a K t
kh kx h z k k a K
x k n n n n
n
x k n n n n
n
n
n
ω ω
ω ω
ωθ
( ) ( ) ( ) ( )
. cos sin
cos cos cosh
, cosh ,
1 0 0
0
e t
h k
h z k k a K t
kh kx h z k k a K t z
x
k xn n n n
n
n
ω
ω θ ω ω
θ
−∞
=
− −
− −
−
= Φ
∴ ∑
(41) The velocity component in x-direction in the following form
268 M.S. Parvin et al.
( ) ( ) ( )
. cos sin
sin cos cosh
cosh
1 0 0
0
e t
h k
h z K k
a t
kh kx h z K k
x a
u
kxn n n
n
n
ω
ω θ ω ω
θ
−∞
=
+ −
− −
∂ = Φ
= ∂ ∑
(42) Now, at the bottom surface,
( ) sin .
cos sin 1
cosh 1
1 0 0
0
e t
h K k
a t
kh kx K
x a
u
kxn n n h
z h
z
n
ω
ω θ ω ω
θ
−∞
=
=
=
= − + ∑
∂ Φ
= ∂
( ) sin .
cos cos 1
cosh 1
1 0 0
0
e t
h Kk k
a t
kh kx Kk
x a
u
kxn n n
n h
z
n
ω
ω θ ω ω
θ
−∞
=
=
= − − ∑
∂
∂
and
( )
( )
− −
− +
∂ =
∂
−
∞
=
−
∞
=
=
∑
∑
t h e
Kk k a t
kh kx Kk
a
t h e
K k a t
kh kx K
x a u u
x k n n n
n
x k n n
n h
z
n n
ω ω
θ ω ω
θ
ω ω
θ ω ω
θ
cos sin cos 1
cosh 1
cos sin sin 1
cosh 1
1 0 0
0
1 0 0
0
( )
( ) sin .
cos cos 1
cosh 1
cos sin sin 1
cosh 1
1 0
1 0
2 2 2 0
− −
− +
=
−
∞
=
∞ −
=
∑
∑
t h e
k k a t kh kx
k a
t h e
a k t kh kx
a K
x k n n n
n
x k n n
n
n n
ω ω
ω ω
ω θ
(43)
At
t = 0
,. cos cosh sin
1
cosh cos sin 1
cosh 1
2 2
2 2 0 2 0
0 0
2 2 2 0
kx kh kx
k K a
kh kx k
a kh kx
a x K
u u
z hω θ
ω θ
=
∂ =
∂
=
(44)
The governing equation of a stream function for the mass transport of the boundary layer is given by Eq. (11) and the boundary conditions on the free surface, water bottom and the flap surface are summarized as
( )
( ) 4 .
Re 0 ,
* 2
2
∂
∂
∂
= ∂
∂ Ψ
∂
x u x w x i
z ω
(45)( )
( )
∂
∂
= −
∂ Ψ
∂
x u u i h i
z x
*
4 3 Re 5
, ω
, where asterisk( ) *
is the complex conjugate.
. 4
3
*x u u
∂
− ∂
= ω
(46)App. Math. and Comp. Intel., Vol. 3 (1), 2014 269
and
( ) .
4 3 Re 5 ,
0
*
∂
∂
− −
=
∂ Ψ
∂
z w w i z i
x ω
(47) Hence Eq. (46) becomes
( )
( )
. cos cosh sin
1 4
3
cos cosh sin
1 4
, 3
2 2 2
0 2 0
2 2
2 2 0 2 0
kx kh kx
k K a
kx kh kx
k K a
h z x
ω θ
ω ω θ
−
=
−
=
∂ Ψ
∂
(48)
Therefore, Eq. (1) can be written as
. cos sin
cos cosh sin
1 4
3
2 2 2
0 2 0 1
kx kx A
kx kh kx
k K a
U
=
−
= θ ω
(49)
where,
k kh a
A
02 2cosh 1 4
3 ω
−
=
(50) Again, the velocity component in z-direction in the following form( ) ( ) ( )
. cos sin
cos sin cosh
sinh
1 0 0
0
e t
h k
h z K k
a t
kh kx h z K k
z a
w
k xn n n
n
n
ω
ω θ ω ω
θ
−∞
=
+ −
− −
−
∂ = Φ
= ∂ ∑
Therefore, at the flap surface,
( ) ( )
. cos sin
cos sin cosh
sinh
1 0 0
0 0
0
t
h k
h z K k
a kh t
h z K k
z a w
n n n
n x
x
θ ω − ω + θ ω − ω
−
∂ = Φ
= ∂
∞
=
=
=
∑
( ) ( )
. cos sin
cos cos cosh
cosh
1 0 0
0
0
t
h k
h z Kk k
a kh t
h z Kk k
z a w
n n n n
n
x
θ ω − ω + θ ω − ω
−
∂ =
∂
∞=
=
∑
and
( ) ( )
( ) ( )
−
− +
−
−
− +
−
∂ =
∂
∞
=
∞
=
∑
∑
h t k
h z Kk k
a kh t
h z Kk k
a
h t k
h z K k
a kh t
h z K k
z a w w
n n n n
n
n n n
n
ω ω
θ ω ω
θ
ω ω
θ ω ω
θ
cos sin cos cos
cosh cosh
cos sin cos sin
cosh sinh
1 0 0
0
1 0 0
0
270 M.S. Parvin et al.
( ) ( )
( ) ( )
−
−
−
−
− −
=
∞
=
∞
=
∑
∑
h t k
h z k k
a kh t
h z k k
a
h t k
h z a k
kh t h z a k
K
n n n n
n
n n n
n
ω ω
ω ω
ω θ
cos sin cos cos
cosh cosh
cos sin cos sin
cosh sinh
1 0
1 0
2 2 2 0
(51)
At
t = 0
( ) ( )
( ) cosh ( ) .
cosh sinh 1
cosh cosh cosh
sinh
2 2
0 2 2 2 0
0 0
2 2 2 0
h z k h z kh k
k a K
kh h z k k
kh a h z a k
z K w w
−
−
=
−
−
∂ =
∂
ω θ
ω θ
(52)
Also Eq. (46) can be written as
( )
∂
∂
− −
=
∂ Ψ
∴ ∂
z w w i z i
x
*
4 3 Re 5 ,
0 ω
z w w
∂
= ∂
*
4 3 ω
( ) cosh ( ) .
cosh sinh 1 4
3
2 2 2
0 2
0
k z h k z h
k kh K
a − −
= θ ω
(53)Therefore, Eq (2) can be written as
( )
( ) ( )
( ) cosh ( ) . sinh
cosh cosh sinh
1 4
3 , 0
2 2 2
0 2 0 1
h z k h z k A
h z k h z kh k
k K a
x W z
−
−
=
−
−
−
=
∂ Ψ
− ∂
=
ω
θ
(54)From Eqs. (49) and (54), mass transport velocity has been formulated.
2.4. Time Average of Horizontal Velocity Component Time average of horizontal velocity u can be expressed as
( ) 1 ( , 0 , ) . ,
0 ,
0
dt t x T u t x u
T
∫
=
(55) Hence Eq. (42) can be written as( ) [ a K ( kx t ) a Ke t ] dt
t T z x
u
kxn n T
n
ω
ω θ ω ω
θ sin sin
, 1 ,
1 0 0
0 0
∞ −
=
∫ − + ∑
=
( )
T x
k n
n
Ke t
a t
kx K T a
n
1 0 2 0 2
0
0
cos cos
1
− −
=
−∞
=
∑ ω
ω θ ω ω
θ = 0 .
App. Math. and Comp. Intel., Vol. 3 (1), 2014 271
Using eigen function expansion, velocity potential has been derived. Then we see that time average of horizontal velocity component is zero, which is same as Dean and Dalrymple [15], who derived some nonlinear properties for water waves of small amplitude.
3. Conclusion
Mass transport velocity in two dimensional wave tank has been studied. Vorticity equation from incompressible Navier-Stokes equation is solved using boundary layer theory and boundary conditions on the free surface, water bottom and the flap surface. Generalising the velocity potential in terms of eigen function expansion, we obtain the velocity components which are related to stream function. Using the given boundary conditions, mass transport velocity has been formulated. Then we see time average of horizontal velocity component is zero at mean water level.
References
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Journal of Fluid Mechanics, 94: 497-517, 1979.
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[3] M.S. Longuet-Higgins .Lagrangian Moments and Mass Transport in Stokes Waves. Journal of Fluid Mechanics, 179: 547-555, 1987
[4] H.K. Chang, J.C. Liou and M. Y. Su. Particle Trajectory and Mass Transport of Finite- Amplitude Waves in Water of Uniform Depth. Elsevier Masson SAS.2006.
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[6] Iskandarani, M. and Liu, P.L.F. Mass Transport in Two-dimensional Wave Tank. J. Fluid Mech. 231: 395- 415, 1991.
[7] Buldakov et-al. New Asymptotic Description of Nonlinear Water Waves in Lagrangian Coordinates. Journal of Fluid Mechanics, 562: 431-444, 2006.
[8] Clamond. On the Lagrangian Description of Steady Surface Gravity Waves. Journal of Fluid Mechanics, 589: 433-454, 2007.
[9] Constantin. On the Deep Water Wave Motion. Journal of Physics A: Mathematical General, 34: 1405-1417, 2001.
[10] Boufermel, A., Joly, N., Lotton, P., Ameri, M., Gusev, V. Velocity of Mass Transport of Model Acoustic Streaming. Numerical Application of Annual Resonator, Acta Acoustica United with Acoustica, 92, No. 2, 219-227(9), 2011.
272 M.S. Parvin et al.
[11] Frode Hoydalsvik. Mass Transport Velocity in Shallow Water Waves Reflected in a Rotating Ocean with a Coastal Boundary. J. Phys. Oceangr. 37, Issue 10, 2429-2445, 2007.
[12] Robert G. Dean and Robert A. Dalrymple (1991), Nonlinear Properties Derivable from Small-Amplitude Waves. Water Wave Mechanics for Engineers and Scientists, 2, WSPC, 1991.