Difference between revisions of "Variable Bottom Topography"

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Wave scattering by a [[Floating Elastic Plate]] on water of Variable Bottom Topography was treated in
 
Wave scattering by a [[Floating Elastic Plate]] on water of Variable Bottom Topography was treated in
[[Wang and Meylan 2002]].
+
[[Wang and Meylan 2002]] and is described in [[Floating Elastic Plate on Variable Bottom Topography]]
  
 
 
\title{The Linear Wave Response of a Floating Thin Plate on Water of
 
Variable Depth}
 
\author{Cynthia D. Wang and Michael H. Meylan \\
 
 
Institute of Information and Mathematical Sciences,\\
 
Massey University, New Zealand}
 
 
 
 
We present a solution for the linear wave forcing of a floating
 
two-dimensional thin plate on water of variable depth. The solution method
 
is based on reducing the problem to a finite domain which contains both the
 
region of variable water depth and the floating thin plate. In this finite
 
region the outward normal derivative of the potential on the boundary is
 
expressed as a function of the potential. This is accomplished by using
 
integral operators for the radiating boundaries and the boundary under the
 
plate. Laplace's equation in the finite domain is solved using the boundary
 
element method and the integral equations are solved by numerical
 
integration. The same discretisation is used for the boundary element method
 
and to integrate the integral equations. The results show that there is a
 
significant region where the solution for a plate with a variable depth
 
differs from the simpler solutions for either variable depth but no plate or
 
a plate with constant depth. Furthermore, the presence of the plate
 
increases the frequency of influence of the variable depth.
 
 
 
=Introduction=
 
 
The linear wave forcing of a floating thin plate can be used to model a wide
 
range of physical systems; for example very large floating structures \cite
 
{Kashiwagihydro98}, sea ice floes [[Squire_Review]] and breakwaters \cite
 
{Stoker}. For this reason it is the one of the best studied hydroelastic
 
problems and several solution methods have been developed. These methods
 
have focused on providing a fast solution and for this reason have
 
exclusively solved for water of constant depth. Furthermore, since all the
 
models tests have been conducted in water of constant depth, only the
 
constant depth solution is required to compare theory and experiment.
 
However, because of the large size of floating hydroelastic structures, it
 
is unlikely that the water depth will be constant under the entire
 
structure. For this reason the effect of a variation in the water depth
 
under a floating thin plate is investigated in this paper.
 
 
As mentioned, the linear wave forcing of a floating thin plate has been
 
extensively studied and standard solution methods have now been developed.
 
These methods are based on expanding the plate motion in basis functions
 
(often thin plate or beam modes) and on solving the equations of motion for
 
the water using a Green function or by a further expansion in modes \cite
 
{Kashiwagihydro98}. A solution of the water equations by either a Green
 
function or an expansion in modes requires the water depth to be constant.
 
Therefore these standard methods are unsuitable to be extended to the case
 
of variable water depth.
 
 
The linear wave scattering by variable depth (or bottom topography) in the
 
absence of a floating plate has been considered by many authors. Two
 
approaches have been developed. The first is analytical and the solution is
 
derived in an almost closed form ([[Porter95]], [[Staziker96]] and
 
[[Porter00]]). However this approach is unsuitable to be generalised to
 
the case when a thin plate is also floating on the water surface because of
 
the complicated free surface boundary condition which the floating plate
 
imposes. The second approach is numerical, an example of which is the method
 
developed by [[Liu82]], in which the boundary element method in a finite
 
region is coupled to a separation of variables solution in the semi-infinite
 
outer domains. This method is well suited to the inclusion of the plate as
 
will be shown. For both the analytic and numerical approach the region of
 
variable depth must be bounded.
 
 
In this paper, a solution method for the linear wave forcing of a two
 
dimensional floating plate on water of variable depth will be derived from
 
[[Liu82]], [[Hazard]] and [[jgrfloe1d]]. The method is based on
 
dividing the water domain into two semi-infinite domains and a finite
 
domain. The finite domain contains both the plate and the region of variable
 
water depth. Laplace's equation in the finite domain is solved by the
 
boundary element method. Laplace's equation in the semi-infinite domains is
 
solved by separation of variables. The solution in the semi-infinite domains
 
gives an integral equation relating the normal derivative of the potential
 
and the potential on the boundary of the finite and semi-infinite domains.
 
The thin plate equation is expressed as an integral equation relating the
 
normal derivative of the potential and the potential under the surface of
 
the plate. The boundary element equations and the integral equations are
 
solved simultaneously using the same discretisation.
 
 
=Problem Formulation=
 
 
We consider a thin plate, floating on the water surface above a sea bed of
 
variable depth, which is subject to an incoming wave. The plate is
 
approximated as infinitely long in the <math>y</math> directions which reduces the
 
problem to two dimensions, <math>x</math> and <math>z</math>. The <math>x</math>-axis is horizontal and the <math>
 
z <math>-axis points vertically up with the free water surface at </math>z=0.</math> The
 
incoming wave is assumed to be travelling in the positive <math>x</math>-direction with
 
a single radian frequency <math>\omega </math>. The theory which will be developed
 
could be extended to oblique incident waves using the standard method \cite
 
{OhkusuISOPE}. However, to keep the treatment straightforward, this will not
 
be done. We assume that the wave amplitude is sufficiently small that the
 
problem can be approximated as linear. From the linearity and the single
 
frequency wave assumption it follows that all quantities can be written as
 
the real part of a complex quantity whose time dependence is <math>e^{-i\omega t}</math>
 
.
 
 
The linear boundary value problem for the water is the following,
 
<center><math>
 
\left.
 
\begin{matrix}{c}
 
\nabla ^{2}\phi =0, \\
 
-\rho g\,w+i\omega \rho \phi =p,\qquad z=0, \\
 
\phi _{n}=0,\qquad z=d\left( x\right) ,
 
\end{matrix}
 
\right\}  (1)
 
</math></center>
 
where <math>\rho </math> is the density of the water, <math>p</math> is the pressure on water
 
surface, <math>w</math> is the displacement of the water surface, <math>g</math> is the
 
gravitational acceleration, <math>d(x)</math> is the water depth and <math>\phi _{n}</math> is the
 
outward normal derivative of the potential. We assume that the water depth
 
is constant outside a finite region, <math>-l<x<l</math>, but allow the depth to be
 
different at either end. Therefore
 
<center><math>
 
d\left( x\right) =\left\{
 
\begin{matrix}{c}
 
-H_{1},\;\;x<-l, \\
 
d\left( x\right) ,\;\;-l<x<l, \\
 
-H_{2},\;\;x>l,
 
\end{matrix}
 
\right.
 
</math></center>
 
where <math>H_{1}</math> and <math>H_{2}</math> are the water depths in the left and right hand
 
domains of constant depth.
 
 
A thin plate, of negligible draft, floats on the surface of the water and
 
occupies the region <math>-L\leq x\leq L\ </math>as is shown in Figure \ref{fig_region}
 
. Without loss of generality, we assume that <math>l</math> is sufficiently large that <math>
 
L<l.</math> For any point on the water surface not under the plate the pressure is
 
the constant atmospheric pressure whose time-dependent part is zero. Under
 
the plate, the pressure and the displacement are related by the
 
Bernoulli-Euler equation
 
<center><math>
 
D\frac{\partial ^{4}w}{\partial x^{4}}-\rho ^{\prime }a\omega
 
^{2}\,w=p,\qquad -L\leq x\leq L= and = z=0,  (2)
 
</math></center>
 
where <math>\rho ^{\prime }</math> is the density of the plate, <math>a</math> is the plate
 
thickness, and <math>D</math> is the bending rigidity of the plate. We assume that the
 
plate edges are free so the bending moment and shear must vanish at both
 
ends of the plate, i.e.
 
<center><math>
 
\frac{\partial ^{2}w}{\partial x^{2}}=\frac{\partial ^{3}w}{\partial x^{3}}
 
=0,\qquad =at= \ x=-L= and = x=L.
 
</math></center>
 
The kinematic boundary condition at the surface allows us to express the
 
displacement as a function of the outward normal derivative of the
 
potential,
 
<center><math>
 
w=\frac{i\phi _{n}}{\omega },\qquad z=0.  (3)
 
</math></center>
 
 
Substituting equations (2) and (3)\ into
 
equation (1), we obtain the following boundary value problem for
 
the potential only,
 
<center><math>
 
\left.
 
\begin{matrix}{c}
 
\nabla ^{2}\phi =0, \\
 
-\rho \left( g\phi _{n}-\omega ^{2}\,\phi \right) =\left\{
 
\begin{matrix}{c}
 
0,\;x\notin \left[ -L,L\right] ,\;z=0, \\
 
D\,\frac{\partial ^{4}\phi _{n}}{\partial x^{4}}-\rho ^{\prime }a\,\omega
 
^{2}\phi _{n},\;x\in \left[ -L,L\right] ,\;z=0,
 
\end{matrix}
 
\right. \\
 
\phi _{n}=0,\qquad z=d\left( x\right) ,
 
\end{matrix}
 
\right\}  (4)
 
</math></center>
 
together with the free plate edge conditions
 
<center><math>
 
\frac{\partial ^{2}\phi _{n}}{\partial x^{2}}=\frac{\partial ^{3}\phi _{n}}{
 
\partial x^{3}}=0,\qquad =at = x=\pm L=, \ \ = z=0.
 
(5)
 
</math></center>
 
 
==Radiation Boundary Conditions==
 
 
Equation (4) is subject to radiation conditions as <math>
 
x\rightarrow \pm \infty .</math> We assume that there is a wave incident from the
 
left which gives rise to a reflected and transmitted wave. Therefore the
 
following boundary conditions for the potential apply as <math>x\rightarrow \pm
 
\infty </math>
 
<center><math>
 
\lim_{x\rightarrow -\infty }\phi \left( x,z\right) =\cosh \left(
 
k_{t}^{\left( 1\right) }\left( z+H_{1}\right) \right) e^{ik_{t}^{\left(
 
1\right) }x}+R\,\cosh \left( k_{t}^{\left( 1\right) }\left( z+H_{1}\right)
 
\right) e^{-k_{t}^{\left( 1\right) }x},  (6)
 
</math></center>
 
and
 
<center><math>
 
\lim_{x\rightarrow \infty }\phi \left( x,z\right) =T\cosh \left(
 
k_{t}^{\left( 2\right) }\left( z+H_{2}\right) \right) e^{k_{t}^{\left(
 
2\right) }x},  (7)
 
</math></center>
 
where <math>R</math> and <math>T</math> are the reflection and transmission coefficients
 
respectively and <math>k_{t}^{\left( j\right) }\,\left( j=1,2\right) </math> are the
 
positive real solutions of the following equation
 
<center><math>
 
gk_{t}^{\left( j\right) }\tanh \left( k_{t}^{\left( j\right) }\,H_{j}\right)
 
=\omega ^{2}.
 
</math></center>
 
 
==(8)Non-dimensionalisation==
 
 
Non-dimensional variables are now introduced. We non-dimensionalise the
 
space variables with respect to the water depth on the left hand side, <math>
 
H_{1},<math> and the time variables with respect to</math>\;\sqrt{g/H_{1}}</math>. The
 
non-dimensional variables, denoted by an overbar, are
 
<center><math>
 
\bar{x}=\frac{x}{H_{1}},\;\bar{z}=\frac{z}{H_{1}},\;\bar{t}=t\sqrt{\frac{g
 
}{H_{1}}},\;=and= \;\bar{\phi}=\frac{1}{H_{1}\sqrt{H_{1}g}}\,\phi .
 
</math></center>
 
Applying this non-dimensionalisation to equation (4)
 
we obtain
 
<center><math>
 
\left.
 
\begin{matrix}{c}
 
\nabla ^{2}\bar{\phi}=0, \\
 
\left( \bar{\phi}_{n}-\nu \bar{\phi}\right) =\left\{
 
\begin{matrix}{c}
 
0,\qquad \bar{x}\notin \left[ -L,L\right] ,\;\bar{z}=0, \\
 
-\beta \,\frac{\partial ^{4}\bar{\phi}_{n}}{\partial \bar{x}^{4}}+\gamma
 
\nu \,\bar{\phi}_{n},\qquad \bar{x}\in \left[ -L,L\right] ,\;\bar{z}=0,
 
\end{matrix}
 
\right. \\
 
\bar{\phi}_{n}=0,\qquad \bar{z}=\bar{d}\left( \bar{x}\right) ,
 
\end{matrix}
 
\right\}  (9)
 
</math></center>
 
where
 
<center><math>
 
\beta =\frac{D}{\rho gH_{1}^{4}},\;\gamma =\frac{\rho ^{\prime }a}{\rho
 
H_{1}},\;=and= \;\nu =\frac{\omega ^{2}H_{1}}{g}.  (10)
 
</math></center>
 
We will refer to <math>\beta </math> as the stiffness, <math>\gamma </math> as the mass and <math>\nu </math>
 
as the wavenumber. The non-dimensional water depth is
 
 
<center><math>
 
\bar{d}\left( \bar{x}\right) =\left\{
 
\begin{matrix}{c}
 
-1,\;\;\bar{x}<-\bar{l}, \\
 
\bar{d}\left( \bar{x}\right) ,\;\;-\bar{l}<\bar{x}<\bar{l}, \\
 
-H,\;\;\bar{x}>\bar{l},
 
\end{matrix}
 
\right.
 
</math></center>
 
where <math>H=H_{2}/H_{1}.</math> Equation (9) is also subject to the
 
non-dimensional free edge conditions of the plate (5) and the
 
radiation conditions (6) and (7). With the
 
understanding that all variables have been non-dimensionalised, from now
 
onwards we omit the overbar.
 
 
=Reduction to a Finite Domain=
 
 
We solve equation (9) by reducing the problem to a finite
 
domain which contains both the region of variable depth and the floating
 
thin plate. This finite domain <math>\Omega =\left\{ -l\leq x\leq l,\;d\left(
 
x\right) \leq z\leq 0\right\} </math> is shown in Figure \ref{fig_region}. We will
 
solve Laplace's equation in <math>\Omega </math> using the boundary element method. To
 
accomplish this we need to express the normal derivative of the potential on
 
the boundary of <math>\Omega \;(\partial \Omega )</math> as a function of the potential
 
on the boundary.
 
 
==Green's Function Solution for the Floating Thin Plate==
 
 
We begin with the boundary condition under the plate which is the following
 
<center><math>
 
\beta \frac{\partial ^{4}\phi _{n}}{\partial x^{4}}-\left( \gamma \nu
 
-1\right) \phi _{n}=\nu \phi ,\;-L\leq x\leq L= and = z=0,  (11)
 
</math></center>
 
together with the free edge boundary conditions (5).
 
Following [[jgrfloe1d]] we can transform equations (5) and
 
(11) to an integral equation using the Green function, <math>g,</math> which
 
satisfies
 
<center><math>
 
\left.
 
\begin{matrix}{c}
 
\beta \frac{\partial ^{4}}{\partial x^{4}}g\left( x,\xi \right) -\left(
 
\gamma \nu -1\right) g\left( x,\xi \right) =\nu \delta \left( x-\xi \right) ,
 
\\
 
\frac{\partial ^{2}}{\partial x^{2}}g\left( x,\xi \right) =\frac{\partial
 
^{3}}{\partial x^{3}}g\left( x,\xi \right) =0,\qquad =at = x=-L,\;x=L.
 
\end{matrix}
 
\right\}
 
</math></center>
 
This gives us the following expression for <math>\phi _{n}</math> as a function of the
 
potential under the plate <math>\phi ,</math>
 
<center><math>
 
\phi _{n}\left( x\right) =\int_{-L}^{L}g\left( x,\xi \right) \;\phi \left(
 
\xi \right) \;d\xi .  (12)
 
</math></center>
 
We will write this in operator notation as <math>\phi _{n}=\mathbf{g}\phi </math> where
 
<math>\mathbf{g}</math> denotes the integral operator with kernel <math>g\left( x,\xi
 
\right) .</math>
 
 
==Solution in the Semi-infinite Domains==
 
 
We now solve Laplace's equation in the semi-infinite domains <math>\Omega
 
^{-}=\left\{ x<-l,\;-1\leq z\leq 0\right\} <math> and </math>\Omega ^{+}=\left\{
 
x>l,\;-H\leq z\leq 0\right\} </math> which are shown in Figure (\ref{fig_region}).
 
Since the water depth is constant in these regions we can solve Laplace's
 
equation by separation of variables. The potential in the region <math>\Omega
 
^{-} </math> satisfies the following equation
 
<center><math>
 
\left.
 
\begin{matrix}{c}
 
\nabla ^{2}\phi =0,\;\;\mathbf{x}\in \Omega ^{-}, \\
 
\phi _{n}-\nu \phi =0,\;\;z=0, \\
 
\phi _{n}=0,\;\;z=-1, \\
 
\phi =\tilde{\phi}\left( z\right) ,\;\;x=-\,l, \\
 
\lim\limits_{x\rightarrow -\infty }\phi \left( x,z\right) =\cosh \left(
 
k_{t}^{\left( 1\right) }\left( z+1\right) \right) e^{ik_{t}^{\left( 1\right)
 
}x} \\
 
+R\,\cosh \left( k_{t}^{\left( 1\right) }\left( z+1\right) \right)
 
e^{-ik_{t}^{\left( 1\right) }x},
 
\end{matrix}
 
\right\}  (13)
 
</math></center>
 
where <math>\mathbf{x}=\left( x,z\right) \ </math>and <math>\tilde{\phi}\left( z\right) </math> is
 
an arbitrary continuous function<math>.</math>\ Our aim is to find the outward normal
 
derivative of the potential on <math>x=-l</math> as a function of <math>\tilde{\phi}\left(
 
z\right) </math>.
 
 
We solve equation (13) by separation of variables \cite{Liu82,
 
Hazard} and obtain the following expression for the potential in the region <math>
 
\Omega ^{-},</math>
 
<center><math>\begin{matrix}
 
\phi \left( x,z\right) &=&\cosh \left( k_{t}^{\left( 1\right) }\left(
 
z+1\right) \right) \,e^{ik_{t}^{\left( 1\right) }x}+R\cosh \left(
 
k_{t}^{\left( 1\right) }\left( z+1\right) \right) \,e^{-ik_{t}^{\left(
 
1\right) }x}  \notag \\
 
&&+\sum_{m=1}^{\infty }\left\langle \tilde{\phi}\left( z\right) ,\tau
 
_{m}^{\left( 1\right) }\left( z\right) \right\rangle \tau _{m}^{\left(
 
1\right) }\left( z\right) e^{k_{m}^{\left( 1\right) }\left( x+l\right) }.
 
(14)
 
\end{matrix}</math></center>
 
The functions <math>\tau _{m}^{\left( 1\right) }\left( z\right) </math> (<math>m\geq 1)</math> are
 
the orthonormal modes given by
 
<center><math>
 
\tau _{m}^{\left( 1\right) }\left( z\right) =\left( \frac{1}{2}+\frac{\sin
 
\left( 2k_{m}^{\left( 1\right) }\,\right) }{4k_{m}^{\left( 1\right) }}
 
\right) ^{-\frac{1}{2}}\cos \left( k_{m}^{\left( 1\right) }\left(
 
z+1\right) \right) ,\;\;m\geq 1.
 
</math></center>
 
The evanescent eigenvalues <math>k_{m}^{\left( 1\right) }</math> are the positive real
 
solutions of the dispersion equation
 
<center><math>
 
-k_{m}^{\left( 1\right) }\,\tan \left( k_{m}^{\left( 1\right) }H_{j}\right)
 
=\nu ,\;\;m\geq 1,  (15)
 
</math></center>
 
ordered by increasing size. The inner product in equation (13) is
 
the natural inner product for the region <math>-1\leq z\leq 0</math> given by
 
<center><math>
 
\left\langle \tilde{\phi}\left( z\right) ,\tau _{m}^{\left( j\right) }\left(
 
z\right) \right\rangle =\int_{-1}^{0}\tilde{\phi}\left( z\right) ,\tau
 
_{m}^{\left( j\right) }\left( z\right) dx.  (16)
 
</math></center>
 
 
The reflection coefficient is determined by taking an inner product of
 
equation (14) with respect to <math>\cosh \left( k_{t}^{\left( 1\right)
 
}\left( z+1\right) \right) .<math> This gives us the following expression for </math>R</math>
 
,
 
<center><math>
 
R=\frac{\left\langle \tilde{\phi}\left( z\right) ,\cosh \left(
 
k_{t}^{\left( 1\right) }\left( z+1\right) \right) \right\rangle }{\frac{1}{2
 
}+\sinh \left( 2k_{t}^{\left( 1\right) }\,\right) /4k_{0}^{\left( 1\right) }}
 
e^{-ik_{t}^{\left( 1\right) }l}-e^{-2ik_{t}^{\left( 1\right) }l}.
 
(17)
 
</math></center>
 
The normal derivative of the potential on the boundary of <math>\Omega ^{-}</math> and <math>
 
\Omega <math> </math>\left( x=-l\right) </math> is calculated using equation (14) and
 
we obtain,
 
<center><math>
 
\left. \phi _{n}\right| _{x=-l}=\mathbf{Q}_{1}\tilde{\phi}\left( z\right)
 
-2ik_{t}^{\left( 1\right) }\cosh \left( k_{t}^{\left( 1\right) }\left(
 
z+1\right) \right) \,e^{-ik_{t}^{\left( 1\right) }l},
 
</math></center>
 
where the outward normal is with respect to the <math>\Omega </math> domain. The
 
integral operator <math>\mathbf{Q}_{1}</math> is given by
 
<center><math>\begin{matrix}
 
\mathbf{Q}_{1}\tilde{\phi}\left( z\right) &=&\sum_{m=1}^{\infty
 
}k_{m}^{\left( 1\right) }\left\langle \tilde{\phi}\left( z\right) ,\tau
 
_{m}^{\left( 1\right) }\left( z\right) \right\rangle \,\tau _{m}^{\left(
 
1\right) }\left( z\right)  (18) \\
 
&&+ik_{t}\frac{\left\langle \tilde{\phi}\left( z\right) ,\cosh \left(
 
k_{t}^{\left( 1\right) }\left( z+1\right) \right) \right\rangle \cosh \left(
 
k_{t}^{\left( 1\right) }\left( z+1\right) \right) }{\frac{1}{2}+\sinh
 
\left( 2k_{t}^{\left( 1\right) }\,\right) /4k_{t}^{\left( 1\right) }}.
 
\notag
 
\end{matrix}</math></center>
 
We can combine the two terms of equation (18) and express <math>\mathbf{Q}
 
_{1}</math> as
 
<center><math>
 
\mathbf{Q}_{1}\tilde{\phi}\left( z\right) =\sum_{m=0}^{\infty }k_{m}^{\left(
 
1\right) }\left\langle \tilde{\phi}\left( z\right) ,\tau _{m}^{\left(
 
1\right) }\left( z\right) \right\rangle \,\tau _{m}^{\left( 1\right) }\left(
 
z\right)  (19)
 
</math></center>
 
where <math>k_{0}^{\left( 1\right) }=ik_{t}^{\left( 1\right) }</math> and
 
<center><math>
 
\tau _{0}^{\left( 1\right) }\left( z\right) =\left( \frac{1}{2}+\frac{\sin
 
\left( 2k_{0}^{\left( 1\right) }\right) }{4k_{0}^{\left( 1\right) }}\right)
 
^{-\frac{1}{2}}\cos \left( k_{0}^{\left( 1\right) }\left( z+1\right)
 
\right) .
 
</math></center>
 
As well as providing a more compact notation, equation (19)
 
will be useful in the numerical calculation of <math>\mathbf{Q}_{1}.</math>
 
 
Similarly, we now consider the potential in the region <math>\Omega ^{+}</math> which
 
satisfies
 
<center><math>
 
\left.
 
\begin{matrix}{c}
 
\nabla ^{2}\phi =0,\;\;\mathbf{x}\in \Omega ^{+}, \\
 
\phi _{n}-\nu \phi =0,\;\;z=0, \\
 
\phi _{n}=0=,= \;\;z=-H, \\
 
\phi =\tilde{\phi}\left( z\right) ,\;\;x=\,l, \\
 
\lim\limits_{x\rightarrow -\infty }\phi \left( x,z\right) =T\cosh \left(
 
k_{t}^{\left( 2\right) }\left( z+H_{2}\right) \right) e^{ik_{t}^{\left(
 
2\right) }x}.
 
\end{matrix}
 
\right\}  (20)
 
</math></center>
 
Solving equation (20) by separation of variables as before we obtain
 
<center><math>
 
\left. \phi _{n}\right| _{x=l}=\mathbf{Q}_{2}\tilde{\phi}\left( z\right) ,
 
</math></center>
 
where the outward normal is with respect to the <math>\Omega </math> domain. The
 
integral operator <math>\mathbf{Q}_{2}</math> is given by
 
<center><math>
 
\mathbf{Q}_{2}\tilde{\phi}\left( z\right) =\sum_{m=0}^{\infty }k_{m}^{\left(
 
2\right) }\left\langle \tilde{\phi}\left( z\right) ,\tau _{m}^{\left(
 
2\right) }\left( z\right) \right\rangle \tau _{m}^{\left( 2\right) }\left(
 
z\right) .  (21)
 
</math></center>
 
The orthonormal modes <math>\tau _{m}^{\left( 2\right) }</math> are given by
 
<center><math>
 
\tau _{m}^{\left( 2\right) }\left( z\right) =\left( \frac{H}{2}+\frac{\sin
 
\left( 2k_{m}^{\left( 2\right) }\,H\right) }{4k_{m}^{\left( 2\right) }}
 
\right) ^{-\frac{1}{2}}\cos \left( k_{m}^{\left( 2\right) }\left(
 
z+H\right) \right) ,
 
</math></center>
 
The eigenvalues <math>k_{m}^{\left( 2\right) }</math> are the positive real solutions <math>
 
\left( m\geq 1\right) <math> and positive imaginary solutions </math>\left( m=0\right) </math>
 
of the dispersion equation
 
<center><math>
 
-k_{m}^{\left( 2\right) }\,\tan \left( k_{m}^{\left( 2\right) }H\right) =\nu
 
.
 
</math></center>
 
The inner product is the same as that given by equation (16)
 
except that the integration is from <math>z=-H</math> to <math>z=0.</math> The transmission
 
coefficient, <math>T,</math> is given by
 
<center><math>
 
T=\frac{\left\langle \tilde{\phi}\left( z\right) ,\cosh \left(
 
k_{t}^{\left( 2\right) }\left( z+1\right) \right) \right\rangle }{\frac{1}{2
 
}+\sinh \left( 2k_{t}^{\left( 2\right) }H\right) /4k_{t}^{\left( 2\right) }}
 
e^{-ik_{t}^{\left( 2\right) }l}.  (22)
 
</math></center>
 
 
==The equation for the finite domain==
 
 
We now consider the finite domain <math>\Omega .</math> In this domain, Laplace's
 
equation is subject to the boundary conditions given by equations (\ref
 
{integral_plate}), (18) and (21) as well as the free surface and
 
sea floor boundary conditions. This gives the following equation for the
 
potential in <math>\Omega ,</math>
 
<center><math>
 
\left.
 
\begin{matrix}{c}
 
\nabla ^{2}\phi =0,\;\;\;\mathbf{x}\in \Omega , \\
 
\phi _{n}=\mathbf{Q}_{1}\phi -2ik_{t}^{\left( 1\right) }\cosh \left(
 
k_{t}^{\left( 1\right) }\left( z+1\right) \right) \,e^{-ik_{t}^{\left(
 
1\right) }l},\;\;\;\mathbf{x}\in \partial \Omega _{1}, \\
 
\phi _{n}=\mathbf{Q}_{2}\phi ,\;\;\;\mathbf{x}\in \partial \Omega _{2}, \\
 
\phi _{n}=\nu \phi ,\;\;\;\mathbf{x}\in \partial \Omega _{3}\cup \partial
 
\Omega _{5}, \\
 
\phi _{n}=\mathbf{g}\phi ,\;\;\;\mathbf{x}\in \partial \Omega _{4}, \\
 
\phi _{n}=0,\;\;\;\mathbf{x}\in \partial \Omega _{6}.
 
\end{matrix}
 
\right\}  (23)
 
</math></center>
 
This boundary value problem is shown in Figure \ref{fig_sigma}. The boundary
 
of <math>\Omega </math> (<math>\partial \Omega )</math> has been divided into the six boundary
 
regions <math>\partial \Omega _{i}</math> shown in the figure. They are respectively,
 
the boundary of <math>\Omega ^{-}</math> and <math>\Omega </math> (<math>\partial \Omega _{1}),</math> the
 
boundary of <math>\Omega ^{+}</math> and <math>\Omega </math> (<math>\partial \Omega _{2}),</math> the free
 
water surface to the left (<math>\partial \Omega _{3}</math>) and right of the plate (<math>
 
\partial \Omega _{5}<math>), the plate (</math>\partial \Omega _{4}</math>), and the sea
 
floor (<math>\partial \Omega _{6}</math>). Equation (23) is the
 
boundary value problem which we will solve numerically.
 
 
=Numerical Solution Method=
 
 
We have reduced the problem to Laplace's equation in a finite domain subject
 
to certain boundary conditions (23). These boundary
 
conditions give the outward normal derivative of the potential as a function
 
of the potential but this is not always a point-wise condition; on some
 
boundaries it is given by an integral equation. We must solve both Laplace's
 
equation and the integral equations numerically. We will solve Laplace's
 
equation by the boundary element method and the integral equations by
 
numerical integration. However, the same discretisation of the boundary will
 
be used for both numerical solutions.
 
 
We begin by applying the boundary element method to equation (\ref
 
{finitedomain}). This gives us the following equation relating the potential
 
and its outward normal derivative on the boundary <math>\partial \Omega </math>
 
<center><math>
 
\frac{1}{2}\phi \left( \mathbf{x}\right) =\int_{\partial \Omega }\left(
 
G_{n}\left( \mathbf{x},\mathbf{x}^{\prime }\right) \phi \left( \mathbf{x}
 
^{\prime }\right) -G\left( \mathbf{x},\mathbf{x}^{\prime }\right) \phi
 
_{n}\left( \mathbf{x}^{\prime }\right) \right) d\mathbf{x}^{\prime },\;\;
 
\mathbf{x}\in \partial \Omega .  (24)
 
</math></center>
 
In equation (24) <math>G\left( \mathbf{x},\mathbf{x}^{\prime
 
}\right) </math> is the free space Green function given by
 
<center><math>
 
G\left( \mathbf{x},\mathbf{x}^{\prime }\right) =\frac{1}{2\pi }\ln \,\left|
 
\mathbf{x}-\mathbf{x}^{\prime }\right| ,  (25)
 
</math></center>
 
and <math>G_{n}\left( \mathbf{x},\mathbf{x}^{\prime }\right) </math> is the outward
 
normal derivative of <math>G</math> (with respect to the <math>\mathbf{x}^{\prime }</math>
 
coordinate).
 
 
We solve equation (24) by a modified constant panel method
 
which reduces it to the following matrix equation
 
<center><math>
 
\frac{1}{2}\vec{\phi}=\mathbf{G}_{n}\vec{\phi}-\mathbf{G}\vec{\phi}_{n}.
 
(26)
 
</math></center>
 
In equation (26) <math>\vec{\phi}\mathcal{\ }</math>and <math>\vec{\phi}
 
_{n}</math> are vectors which approximate the potential and its normal derivative
 
around the boundary <math>\partial \Omega </math>, and <math>\mathbf{G}</math> and <math>\mathbf{G}_{n}</math>
 
are matrices corresponding to the Green function and the outward normal
 
derivative of the Green function respectively. The method used to calculate
 
the elements of the matrices <math>\mathbf{G}</math> and <math>\mathbf{G}_{n}</math> will be
 
discussed in section \ref{Green}.
 
 
The outward normal derivative of the potential, <math>\vec{\phi}_{n},</math> and the
 
potential, <math>\vec{\phi},</math> are related by the conditions on the boundary <math>
 
\partial \Omega </math> in equation (23). This can be expressed as
 
<center><math>
 
\vec{\phi}_{n}=\mathbf{A}\,\vec{\phi}-\vec{f},  (27)
 
</math></center>
 
where <math>\mathbf{A}</math> is the block diagonal matrix given by
 
<center><math>
 
\mathbf{A}\mathbb{=}\left[
 
\begin{matrix}{cccccc}
 
\mathbf{Q}_{1} &  &  &  &  &  \\
 
& \mathbf{Q}_{2} &  &  &  &  \\
 
&  & \nu \,\mathbf{I} &  &  &  \\
 
&  &  & \mathbf{g} &  &  \\
 
&  &  &  & \nu \,\mathbf{I} &  \\
 
&  &  &  &  & 0
 
\end{matrix}
 
\right] ,  (28)
 
</math></center>
 
<math>\mathbf{Q}_{1}</math>, <math>\mathbf{Q}_{2}</math>, and <math>\mathbf{g}</math> are matrix
 
approximations of the integral operators of the same name and <math>\vec{f}</math> is
 
the vector
 
<center><math>
 
\vec{f}=\left[
 
\begin{matrix}{c}
 
2ik_{t}^{\left( 1\right) }\cosh \left( k_{t}^{\left( 1\right) }\left(
 
z+1\right) \right) \,e^{ik_{t}^{\left( 1\right) }l} \\
 
0 \\
 
\vdots \\
 
0
 
\end{matrix}
 
\right] .  (29)
 
</math></center>
 
\ The methods used to construct the matrices <math>\mathbf{Q}_{1},\mathbf{Q}_{2}</math>
 
, and <math>\mathbf{g}</math> will be described in sections 31 and \ref
 
{numericalg} respectively.
 
 
Substituting equation (27) into equation (\ref
 
{panelEqn_boundary}) we obtain the following matrix equation for the
 
potential
 
<center><math>
 
\left( \frac{1}{2}-\mathbf{G}_{n}+\mathbf{GA}\right) \vec{\phi}=\mathbf{G}
 
\vec{f}
 
</math></center>
 
which can be solved straightforwardly. The reflection and transmission
 
coefficients are calculated from <math>\vec{\phi}</math> using equations (\ref
 
{reflection}) and (22) respectively.
 
 
==Numerical Calculation of <math>\mathbf{G==</math> and <math>\mathbf{G}_{n}</math>\label
 
{Green}}
 
 
The boundary element equation (24) is solved numerically by
 
a modified constant panel method. In this method, the boundary is divided
 
into panels over which the potential, <math>\phi ,</math> or its outward normal
 
derivative, <math>\phi _{n},</math> are assumed to be constant. The free-space Green's
 
function, <math>G,</math> and its normal derivative, <math>G_{n}</math> are more rapidly varying
 
and have a singularity at <math>\mathbf{x}=\mathbf{x}^{\prime }</math>. For this
 
reason, over each panel, while <math>\phi </math> and <math>\phi _{n}</math> are assumed constant,
 
<math>G</math> and <math>G_{n}</math> are integrated exactly. For example, we use the following
 
approximation to calculate the integral of <math>G</math> and <math>\phi </math> over a single
 
panel
 
<center><math>
 
\int_{\mathbf{x}_{i}-h/2}^{\mathbf{x}_{i}+h/2}G\left( \mathbf{x},\mathbf{x}
 
^{\prime }\right) \phi \left( \mathbf{x}^{\prime }\right) d\mathbf{x}
 
^{\prime }\approx \phi \left( \mathbf{x}_{i}\right) \int_{\mathbf{x}
 
_{i}-h/2}^{\mathbf{x}_{i}+h/2}G\left( \mathbf{x},\mathbf{x}^{\prime }\right)
 
d\mathbf{x}^{\prime },  (30)
 
</math></center>
 
where <math>\mathbf{x}_{i}</math> is the midpoint of the panel and <math>h</math> is the panel
 
length. The integral on the right hand side of equation (30),
 
because of the simple structure of <math>G</math>, can be calculated exactly.
 
 
==Numerical Calculation of <math>\mathbf{Q==_{1}</math> and <math>\mathbf{Q}_{2}
 
(31)</math>}
 
 
We will discuss the numerical approximation of the operator <math>\mathbf{Q}_{1}</math>
 
. The operator <math>\mathbf{Q}_{2}</math> is approximated in a similar fashion. We
 
begin with equation (19) truncated to a finite number (<math>N</math>) of
 
evanescent modes,
 
<center><math>
 
\mathbf{Q}_{1}\phi =\sum_{m=0}^{N}k_{m}^{\left( 1\right) }\left\langle \phi
 
\left( z\right) ,\tau _{m}^{\left( 1\right) }\left( z\right) \right\rangle
 
\tau _{m}^{\left( 1\right) }\left( z\right) .
 
</math></center>
 
We calculate the inner product
 
<center><math>
 
\left\langle \phi \left( z\right) ,\tau _{m}^{\left( 1\right) }\left(
 
z\right) \right\rangle =\int\nolimits_{-1}^{0}\phi \left( z\right) \,\tau
 
_{m}^{\left( 1\right) }\left( z\right) \,dz
 
</math></center>
 
with the same panels as we used to approximate the integrals of the Green
 
function and its normal derivative in subsection \ref{Green}. Similarly, we
 
assume that <math>\phi </math> is constant over each panel and integrate <math>\tau
 
_{m}^{\left( 1\right) }\left( z\right) </math> exactly. This gives us the
 
following matrix factorisation of <math>\mathbf{Q}_{1},</math>
 
<center><math>
 
\mathbf{Q}_{1}\,\vec{\phi}=\mathbf{S}\,\mathbf{R}\,\vec{\phi}.
 
</math></center>
 
The components of the matrices <math>\mathbf{S}</math> and <math>\mathbf{R}</math> are
 
<center><math>\begin{matrix}
 
s_{im} &=&\tau _{m}^{\left( 1\right) }\left( z_{i}\right) , \\
 
r_{mj} &=&k_{m}^{\left( 1\right) }\int_{z_{j}-h/2}^{z_{j}+h/2}\tau
 
_{m}^{\left( 1\right) }\left( s\right) ds
 
\end{matrix}</math></center>
 
where <math>z_{j}</math> is the value of the <math>z</math> coordinate in the centre of the panel
 
and <math>h</math> is the panel length. The integral operator <math>\mathbf{Q}_{2}</math> is
 
approximated by a matrix in exactly the same manner.
 
 
==Numerical Calculation of <math>\mathbf{g(32)==</math>}
 
 
The method used to approximate <math>\mathbf{g}</math> by a matrix is similar to the
 
methods used for <math>\mathbf{Q}_{1}</math> and <math>\mathbf{Q}_{2}</math> and follows \cite
 
{jgrfloe1d} with some modification. The Green function for the plate can be
 
expressed as
 
<center><math>
 
g\left( x,\xi \right) =\left\{
 
\begin{matrix}{c}
 
A_{1}e^{i\alpha x}+B_{1}e^{-i\alpha x}+C_{1}e^{\alpha x}+D_{1}e^{-\alpha
 
x},\qquad x<\xi , \\
 
A_{2}e^{i\alpha x}+B_{2}e^{-i\alpha x}+C_{2}e^{\alpha x}+D_{2}e^{-\alpha
 
x},\qquad x>\xi ,
 
\end{matrix}
 
\right.
 
</math></center>
 
where the coefficients are determined by solving a linear system \cite
 
{jgrfloe1d}. Again the same panels are used to approximate the integral
 
operator by a matrix as were used for the boundary integral equation (\ref
 
{integral_eqn}). Over each panel we assume that the potential is constant
 
and integrate the Green function <math>g</math> exactly.
 
 
=Results=
 
 
We will now present some results, concentrating on comparing the reflection
 
coefficient for constant and variable depth profiles. This will allow us to
 
determine when the variable depth profile has a significant effect. To
 
reduce the number of figures we restrict ourselves to four values of the
 
stiffness <math>\beta </math> and two variable depth profiles.
 
 
==Profiles for the variable depth==
 
 
We will consider two different profiles for the variable depth. The first
 
will be the profile which was used by [[Staziker96]]. This corresponds to
 
a rise from a uniform depth to a maximum height of half the uniform depth at
 
<math>x=0</math>. The formula for this profile is the following
 
<center><math>
 
d\left( x\right) =\left\{
 
\begin{matrix}{c}
 
-1,\;\;x<-l, \\
 
-\left( \frac{1}{2}\left( \frac{x+l}{l}\right) ^{2}-\frac{x+l}{l}
 
+1\right) ,\;\;-l<x<l, \\
 
-1,\;\;x>l.
 
\end{matrix}
 
\right.  (33)
 
</math></center>
 
Following [[Staziker96]] we will refer to this variable depth profile as
 
the ''hump. ''
 
 
In the second profile the depth rises linearly. The depth in the right hand
 
region is half the depth in the left hand region. The formula for this
 
profile is
 
<center><math>
 
d\left( x\right) =\left\{
 
\begin{matrix}{c}
 
-1,\;\;x<-l, \\
 
\frac{x+l}{4l}-1,\;\;-l<x<l, \\
 
-\frac{1}{2},\;\;x>l.
 
\end{matrix}
 
\right.  (34)
 
</math></center>
 
We will refer to this variable depth profile as the ''simple slope'' .
 
 
==Convergence study==
 
 
We now present a convergence study. Since we have two parameters, the panel
 
size used to discretise the boundary and the number of evanescent modes (<math>N</math>
 
) used to approximate the integral equations <math>\mathbf{Q}_{1}</math> and <math>\mathbf{Q}
 
_{2},</math> we must present two convergence studies considering each parameter
 
separately. We begin by considering the panel size used to discretise the
 
boundary. We expect that the panel size should be proportional to the
 
wavelength and therefore inversely proportional to the wavenumber <math>
 
k_{t}^{\left( 1\right) }</math> (assuming that the water depth at either end is of
 
a similar size). We therefore use the following formula for the panel size
 
<center><math>
 
=panel size = =\frac{1}{\kappa \,k_{t}^{\left( 1\right) }},
 
</math></center>
 
where <math>\kappa </math> is a constant of proportionality which will be determined
 
from the convergence study. Table 35 shows the absolute value
 
of the reflection coefficient for a plate of length <math>L=2.5,</math> stiffness <math>
 
\beta =1,<math> and mass </math>\gamma =0<math> for </math>\nu =1,</math> 2, and 3 for a constant depth
 
and for the hump with <math>l=2.5.</math> The number of evanescent modes, <math>N,</math> was
 
fixed to be 5. Three values of <math>\kappa </math> were considered, <math>\kappa =10,</math> 20,
 
and 40. The results in Table 35 show that good convergence is
 
achieved when <math>\kappa =20.</math>
 
 
Table 37 shows a similar convergence study for the number of
 
evanescent modes. We have considered <math>0,</math> 5 and <math>10</math> evanescent modes (<math>N</math>)
 
and fixed <math>\kappa </math> to be <math>\kappa =20</math>. All other parameters as the same as
 
those in Table 35. The results in Table 37 show
 
that good convergence is achieved when the number of modes is 5. For all
 
subsequent calculations the panel size will be determined by setting <math>\kappa
 
=20<math> and </math>N=5.</math>
 
 
==Comparison with existing results==
 
 
Before presenting our results for a plate on water of variable depth we will
 
make comparisons with two results from the literature. This is to establish
 
that our method gives the correct solution for the simpler cases of either
 
variable depth but no plate, or a plate floating on constant depth. We begin
 
by comparing our results with [[Staziker96]] who solved for wave
 
scattering by variable depth only. One problem which they solved was to
 
determine the absolute value of the reflection coefficient for a hump depth
 
profile with fixed frequency <math>\nu =1</math> and variable hump length <math>l.</math> The
 
solution to this problem by our method is shown in Figure (\ref{staziker1.ps}
 
). This figure is identical to Figure 2 in [[Staziker96]] (p. 290) which
 
establishes that our method gives the correct solution for a variable depth
 
in the absence of the plate.
 
 
The second comparison is with [[jgrfloe1d]] in which the problem of a
 
thin plate on water of constant depth was solved (to model an ice floe). One
 
problem which they solved was the absolute value of the reflection
 
coefficient as a function of plate length for fixed <math>\nu .</math> The dimensional
 
parameters which they used were, density <math>\rho ^{\prime }=922.5\,</math>kgm<math>^{-3},</math>
 
thickness <math>h=1</math>m, and bending rigidity <math>D=</math>5.4945<math>\times 10^{8}</math>kgm<math>^{2}</math>s<math>
 
^{-2}.<math> The water density was 1025kgm</math>^{-3}</math> and the incoming wave was
 
chosen to have wavelength <math>100</math>m. The solution to this problem by our method
 
is shown in Figure (\ref{fig_mike_refl}). This figure is identical to Figure
 
3 in [[jgrfloe1d]] (p. 895) which establishes that our method gives the
 
correct result for a plate on water of constant depth.
 
 
==Reflection==
 
 
We will consider the absolute value of the reflection coefficient as a
 
function of wavenumber <math>\nu </math> for various values of the parameters. Figure (
 
\ref{plot4hump}) shows the absolute value of the reflection coefficient as a
 
function of <math>\nu </math> with <math>\beta =0.01,</math> <math>0.1,</math> 1 and 10 and <math>\gamma =0</math> for
 
the hump depth profile. Both the length of the hump and the length of the
 
plate were fixed to be <math>l=L=2.5</math>. The solution for the plate and hump (solid
 
line), plate with constant depth (dashed line) and hump only (dotted line)
 
are shown. The two simpler solutions are drawn so that the full solution may
 
be compared to these simpler cases. Figure (\ref{plot4hump}) shows the
 
existence of two asymptotic regimes. When <math>\nu </math> is small (low frequency or
 
large wavelength)\ the reflection is dominated by the hump and the plate is
 
transparent. For large <math>\nu </math> the reflection is dominated by the plate and
 
the hump is transparent. As the value of the stiffness <math>\beta </math> is increased
 
the hump dominated region becomes smaller and the plate dominated region
 
becomes larger. This not unexpected because increasing the value of <math>\beta </math>
 
increases the influence of the plate. It is apparent that, especially for
 
smaller values of stiffness, there is a large region where the hump and
 
plate solution is significantly different from the plate only solution, even
 
though the hump only reflection is practically zero. This is because the
 
wavelength under the plate is larger than the open water wavelength so the
 
depth variation is felt more strongly when the plate is present.
 
 
Figure (\ref{plot4plane}) is equivalent to Figure (\ref{plot4hump}) except
 
that the depth profile is the simple slope and the results are also very
 
similar<math>.</math> Figure (\ref{plot4hump_gamma}) is equivalent to Figure (\ref
 
{plot4hump}) except that the value of stiffness is fixed (<math>\beta =0.1)</math> and
 
the value of <math>\gamma </math> is varied. This figure shows that for realistic
 
(small) values of <math>\gamma </math> this parameter is not significant. This explains
 
why <math>\gamma </math> is often neglected (e.g. [[OhkusuISOPE]]) and why we have
 
chosen <math>\gamma =0</math> for Figures (\ref{plot4hump}) and (\ref{plot4plane}).
 
 
Figure (\ref{plot4ahump}) is equivalent to figure (\ref{plot4hump}) except
 
that the hump has been moved by <math>L</math> to the left so that the minimum depth is
 
directly underneath the left (incoming) end of the plate. Comparing figure (
 
\ref{plot4ahump}) with figure (\ref{plot4ahump}) we see that moving the hump
 
has made a significant change to the reflection coefficient for low
 
frequencies, especially as the stiffness <math>\beta </math> is increased.
 
 
==Displacements==
 
 
Finally we investigate the displacement of the plate for some of the regimes
 
we have considered. We present the displacement for the variable and
 
constant depth profiles so that we may compare the effect of the variable
 
depth. We divide the displacement by <math>i\omega /k_{t}^{\left( 1\right) }\sinh
 
\left( k_{t}^{\left( 1\right) }\right) </math> so that the incoming wave now has
 
unit amplitude in displacement at the water surface. Figure (\ref
 
{deflbeta4hump_nu05}) shows the displacement of the plate for <math>\nu =0.5</math> and
 
<math>\beta =0.01,</math> <math>0.1,</math> 1 and 10 and <math>\gamma =0.</math> The plate length is <math>L=2.5</math>.
 
The solid line is the real part of the displacement and the dotted line is
 
the imaginary part of the displacement. The thicker line is the solution
 
with the hump depth profile (<math>l=2.5)</math> and the thinner line is the solution
 
with a constant depth. It is apparent from this figure, that the bending of
 
the plate is increased by the presence of the hump, but that this effect is
 
not very strong. Figures (\ref{deflbeta4hump_nu1}) and (\ref
 
{deflbeta4hump_nu2}) are identical to Figure (\ref{deflbeta4hump_nu05})
 
except that <math>v=1</math> and <math>\nu =2</math> respectively. These figures also show only a
 
slight increase in the bending of the plate due to the hump. It appears
 
that, while the variable depth does have a significant effect on the
 
reflection coefficient, the effect on the plate displacement is not
 
necessarily as strong.
 
 
=Summary=
 
 
We have presented a solution for the linear wave forcing of a floating thin
 
plate on water of variable depth. The solution method was based on reducing
 
the problem to a finite domain which contained both the region of variable
 
water depth and the floating thin plate. In this finite region the outward
 
normal derivative of the potential around the boundary was expressed as a
 
function of the potential. This was accomplished by using integral operators
 
for the boundary under the plate and the radiating boundaries. The integral
 
operator for the plate was calculated using a Green function as described in
 
[[jgrfloe1d]]. The integral operators for the radiation boundary
 
conditions were calculated by solving Laplace's equation in the
 
semi-infinite outer domains using separation of variables as described in
 
[[Liu82, Hazard]]. Laplace's equation in the finite domain was solved
 
using the boundary element method.
 
 
The results showed that, for certain parameter regimes, there was
 
significant difference between the absolute value of the reflection
 
coefficient for the variable depth and constant depth profiles. Furthermore,
 
the region of influence of the variable depth was increased by the presence
 
of the plate due to the increased wavelength under the plate. Finally, there
 
was a slight increase in the bending of the plate due to the presence of the
 
variable depth profile.
 
 
\bibliographystyle{IEEE}
 
\bibliography{mike,others}
 
\pagebreak
 
 
=Tables=
 
 
 
 
\begin{table}[h] \centering
 
 
(35)
 
\begin{tabular}{lll}
 
<math>\nu =1</math> &  &  \\ \hline
 
\multicolumn{1}{|c}{<math>\kappa </math>} & \multicolumn{1}{|c}{plate only} &
 
\multicolumn{1}{|c|}{plate and hump} \\ \hline
 
\multicolumn{1}{|c}{10} & \multicolumn{1}{|c}{0.2983746166} &
 
\multicolumn{1}{|c|}{0.2491046427} \\ \hline
 
\multicolumn{1}{|c}{20} & \multicolumn{1}{|c}{0.2957175612} &
 
\multicolumn{1}{|c|}{0.2470511349} \\ \hline
 
\multicolumn{1}{|c}{40} & \multicolumn{1}{|c}{0.2948480461} &
 
\multicolumn{1}{|c|}{0.2465182527} \\ \hline
 
<math>\nu =2</math> &  &  \\ \hline
 
\multicolumn{1}{|c}{<math>\kappa </math>} & \multicolumn{1}{|c}{plate only} &
 
\multicolumn{1}{|c|}{plate and hump} \\ \hline
 
\multicolumn{1}{|c}{10} & \multicolumn{1}{|c}{0.3457203891} &
 
\multicolumn{1}{|c|}{0.1934227806} \\ \hline
 
\multicolumn{1}{|c}{20} & \multicolumn{1}{|c}{0.3461627544} &
 
\multicolumn{1}{|c|}{0.1947144005} \\ \hline
 
\multicolumn{1}{|c}{40} & \multicolumn{1}{|c}{0.3463681703} &
 
\multicolumn{1}{|c|}{0.1952205755} \\ \hline
 
<math>\nu =3</math> &  &  \\ \hline
 
\multicolumn{1}{|c}{<math>\kappa </math>} & \multicolumn{1}{|c}{plate only} &
 
\multicolumn{1}{|c|}{plate and hump} \\ \hline
 
\multicolumn{1}{|c}{10} & \multicolumn{1}{|c}{0.0277944414} &
 
\multicolumn{1}{|c|}{0.2605833203} \\ \hline
 
\multicolumn{1}{|c}{20} & \multicolumn{1}{|c}{0.0249319083} &
 
\multicolumn{1}{|c|}{0.2568361963} \\ \hline
 
\multicolumn{1}{|c}{40} & \multicolumn{1}{|c}{0.0236686063} &
 
\multicolumn{1}{|c|}{0.2550926942} \\ \hline
 
\end{tabular}
 
\caption{<math>\left|R\right|</math> for <math>\kappa</math> = 10, 20, and 40 and
 
<math>\nu </math> = 1,2, and 3 for the plate only and the plate and hump.
 
<math>\beta=1</math>, <math>\gamma =0</math> and 5 evanscent modes are
 
used. (36)}
 
 
 
\end{table}
 
 
\pagebreak
 
 
 
 
\begin{table}[t] \centering
 
 
(37)
 
\begin{tabular}{ccc}
 
<math>\nu =1</math> &  &  \\ \hline
 
\multicolumn{1}{|c}{<math>N</math>} & \multicolumn{1}{|c}{plate only} &
 
\multicolumn{1}{|c|}{plate and hump} \\ \hline
 
\multicolumn{1}{|c}{0} & \multicolumn{1}{|c}{0.2934754434} &
 
\multicolumn{1}{|c|}{0.2448842047} \\ \hline
 
\multicolumn{1}{|c}{5} & \multicolumn{1}{|c}{0.2957175612} &
 
\multicolumn{1}{|c|}{0.2470511349} \\ \hline
 
\multicolumn{1}{|c}{10} & \multicolumn{1}{|c}{0.2957697025} &
 
\multicolumn{1}{|c|}{0.2470814786} \\ \hline
 
<math>\nu =2</math> &  &  \\ \hline
 
\multicolumn{1}{|c}{<math>N</math>} & \multicolumn{1}{|c}{plate only} &
 
\multicolumn{1}{|c|}{plate and hump} \\ \hline
 
\multicolumn{1}{|c}{0} & \multicolumn{1}{|c}{0.3392954189} &
 
\multicolumn{1}{|c|}{0.2021691049} \\ \hline
 
\multicolumn{1}{|c}{5} & \multicolumn{1}{|c}{0.3461627544} &
 
\multicolumn{1}{|c|}{0.1947144005} \\ \hline
 
\multicolumn{1}{|c}{10} & \multicolumn{1}{|c}{0.3459741914} &
 
\multicolumn{1}{|c|}{0.1944525347} \\ \hline
 
<math>\nu =3</math> &  &  \\ \hline
 
\multicolumn{1}{|c}{<math>N</math>} & \multicolumn{1}{|c}{plate only} &
 
\multicolumn{1}{|c|}{plate and hump} \\ \hline
 
\multicolumn{1}{|c}{0} & \multicolumn{1}{|c}{0.0262065602} &
 
\multicolumn{1}{|c|}{0.2296877448} \\ \hline
 
\multicolumn{1}{|c}{5} & \multicolumn{1}{|c}{0.0249319083} &
 
\multicolumn{1}{|c|}{0.2568361963} \\ \hline
 
\multicolumn{1}{|c}{10} & \multicolumn{1}{|c}{0.0259483771} &
 
\multicolumn{1}{|c|}{0.2578144528} \\ \hline
 
\end{tabular}
 
\caption{<math>\left|R\right|</math> for 0, 5, and 10 evanescent modes (<math>N</math>)
 
and <math>\nu </math> = 1,2, and 3 for the plate only and the plate and hump.
 
<math>\beta=1</math>, <math>\gamma =0</math> and
 
<math>\kappa = 20</math>.(38)}
 
 
 
\end{table}
 
  
  

Revision as of 08:52, 15 August 2006

A problem in which the scattering comes from a variation in the bottom topography.

Wave scattering by a Floating Elastic Plate on water of Variable Bottom Topography was treated in Wang and Meylan 2002 and is described in Floating Elastic Plate on Variable Bottom Topography