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		<id>https://www.wikiwaves.org/index.php?title=Floating_Elastic_Plate&amp;diff=2751</id>
		<title>Floating Elastic Plate</title>
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		<updated>2006-06-09T03:38:37Z</updated>

		<summary type="html">&lt;p&gt;Hyuck: /* Equations of Motion */&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;= Introduction =&lt;br /&gt;
&lt;br /&gt;
The floating elastic plate is one of the best studied problems in hydroelasticity. It can be used to model a range of&lt;br /&gt;
physical structures such as a floating break water, an ice floe or a [[VLFS]]). The equations of motion were formulated&lt;br /&gt;
more than 100 years ago and a discussion of the problem appears in [[Stoker 1957]]. The problem can&lt;br /&gt;
be divided into the two and three dimensional formulations which are closely related. The plate is assumed to be isotropic while the water motion is irrotational and inviscid.&lt;br /&gt;
&lt;br /&gt;
The solution methods are divided up into those for [[Two-Dimensional Floating Elastic Plate]] and those for&lt;br /&gt;
a [[Three-Dimensional Floating Elastic Plate]]&lt;br /&gt;
&lt;br /&gt;
= Two Dimensional Problem =&lt;br /&gt;
&lt;br /&gt;
== Equations of Motion ==&lt;br /&gt;
&lt;br /&gt;
When considering a two dimensional problem, the &amp;lt;math&amp;gt;y&amp;lt;/math&amp;gt; variable is dropped and the plate is regarded as a beam. There are various beam theories that can be used to describe the motion of the beam. The simplest theory is the [[Bernoulli-Euler Beam]] which is commonly used in the two dimensional hydroelastic analysis. Other beam theories include the [[Timoshenko Beam]] theory and [[Reddy-Bickford Beam]] theory where shear deformation of higher order is considered. &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
For a Bernoulli-Euler beam on the surface of the water, the equation of motion is given&lt;br /&gt;
by the following&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;D\frac{\partial^4 \eta}{\partial x^4} + \rho_i h \frac{\partial^2 \eta}{\partial t^2} = p&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where &amp;lt;math&amp;gt;D&amp;lt;/math&amp;gt; is the flexural rigidity, &amp;lt;math&amp;gt;\rho_i&amp;lt;/math&amp;gt; is the density of the beam,&lt;br /&gt;
&amp;lt;math&amp;gt;h&amp;lt;/math&amp;gt; is the thickness of the beam (assumed constant), &amp;lt;math&amp;gt; p&amp;lt;/math&amp;gt; is the pressure&lt;br /&gt;
and &amp;lt;math&amp;gt;\eta&amp;lt;/math&amp;gt; is the beam vertical displacement. &lt;br /&gt;
&lt;br /&gt;
The edges of the plate satisfy the natural boundary condition (i.e. free-edge boundary conditions). &lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;\frac{\partial^2 \eta}{\partial x^2} = 0, \,\,\frac{\partial^3 \eta}{\partial x^3} = 0&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
at the edges of the plate.&lt;br /&gt;
&lt;br /&gt;
The pressure is given by the linearised Bernoulli equation at the wetted surface (assuming zero&lt;br /&gt;
pressure at the surface), i.e.&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;p = \rho g \frac{\partial \phi}{\partial z} + \rho \frac{\partial \phi}{\partial t}&amp;lt;/math&amp;gt; &lt;br /&gt;
&lt;br /&gt;
where &amp;lt;math&amp;gt;\rho&amp;lt;/math&amp;gt; is the water density and &amp;lt;math&amp;gt;g&amp;lt;/math&amp;gt; is gravity, and &amp;lt;math&amp;gt;\phi&amp;lt;/math&amp;gt;&lt;br /&gt;
is the velocity potential. The velocity potential is governed by Laplace&#039;s equation through out&lt;br /&gt;
the fluid domain subject to the free surface condition and the condition of no flow through the&lt;br /&gt;
bottom surface. If we denote the beam-covered (or possible multiple beams covered) region of the fluid by &amp;lt;math&amp;gt;P&amp;lt;/math&amp;gt; and the free surface by &amp;lt;math&amp;gt;F&amp;lt;/math&amp;gt; the equations of motion for the&lt;br /&gt;
[[Frequency Domain Problem]] with frequency &amp;lt;math&amp;gt;\omega&amp;lt;/math&amp;gt; for water of&lt;br /&gt;
[[Finite Depth]] are the following. At the surface&lt;br /&gt;
we have the dynamic condition &lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;D\frac{\partial^4 \eta}{\partial x^4} +\left(\rho g- \omega^2 \rho_i h \right)\eta = &lt;br /&gt;
 i\omega \rho \phi, \, z=0, \, x\in P&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;0= &lt;br /&gt;
\rho g \frac{\partial \phi}{\partial z} + i\omega \rho \phi, \, x\in F&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
and the kinematic condition&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;\frac{\partial\phi}{\partial z} = i\omega\eta&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
The equation within the fluid is governed by [[Laplace&#039;s Equation]] &lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;\nabla^2\phi =0 &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
and we have the no-flow condition through the bottom boundary &lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;\frac{\partial \phi}{\partial z} = 0, \, z=-h&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
(so we have a fluid of constant depth with the bottom surface at &amp;lt;math&amp;gt;z=-h&amp;lt;/math&amp;gt; and the&lt;br /&gt;
free surface or plate covered surface are at &amp;lt;math&amp;gt;z=0&amp;lt;/math&amp;gt;). &lt;br /&gt;
&amp;lt;math&amp;gt; g &amp;lt;/math&amp;gt; is the acceleration due to gravity,  &amp;lt;math&amp;gt; \rho_i &amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt; \rho &amp;lt;/math&amp;gt; &lt;br /&gt;
are the densities of the plate and the water respectively, &amp;lt;math&amp;gt; h &amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt; D &amp;lt;/math&amp;gt;&lt;br /&gt;
the thickness and flexural rigidity of the plate.&lt;br /&gt;
&lt;br /&gt;
== Solution Methods ==&lt;br /&gt;
&lt;br /&gt;
There are many different methods to solve the corresponding equations ranging from highly analytic such&lt;br /&gt;
as the [[Wiener-Hopf]] to very numerical based on [[Eigenfunction Matching Method]] which are&lt;br /&gt;
applicable and have advantages in different situations. We describe here some of the solutions&lt;br /&gt;
which have been developed grouped by problem&lt;br /&gt;
&lt;br /&gt;
=== Single Crack ===&lt;br /&gt;
&lt;br /&gt;
The simplest problem to consider is one where there are only two semi-infinite plates of identical properties separated by a crack. A related problem in acoustics was considered by [[Kouzov 1963]] who used an integral representation of the problem to solve it explicitly using the Riemann-Hilbert technique. Recently the crack problem has been considered by [[Squire and Dixon 2000]] and [[Williams and Squire 2002]] using a Green function method applicable to infinitely deep water and they obtained simple expressions for the reflection and transmission coefficients. [[Squire and Dixon 2001]] extended the single crack problem to a multiple crack problem in which the semi-infinite regions are separated by a region consisting of a finite number of plates of finite size with all plates having identical properties. [[Evans and Porter 2005]] further considered the multiple crack problem for finitely deep water and provided an explicit solution.&lt;br /&gt;
&lt;br /&gt;
We present here the solution of [[Evans and Porter 2005]] for the simple&lt;br /&gt;
case of a single crack with waves incident from normal (they also considered multiple cracks&lt;br /&gt;
and waves incident from different angles). &lt;br /&gt;
The solution of [[Evans and Porter 2005]] expresses the potential&lt;br /&gt;
&amp;lt;math&amp;gt;\phi&amp;lt;/math&amp;gt; in terms of a linear combination of the incident wave and certain source functions located at the crack.&lt;br /&gt;
Along with satisfying the field and boundary conditions, these source functions satisfy the jump conditions in the displacements and gradients across the crack.&lt;br /&gt;
They first define &amp;lt;math&amp;gt;\chi(x,z)&amp;lt;/math&amp;gt; to be the Two-Dimensional solution to the [[Free-Surface Green Function for a Floating Elastic Plate]]&lt;br /&gt;
given by&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
\chi(x,z) = -i\sum_{n=-2}^\infty\frac{\sin{(k_n h)}\cos{(k(n)(z-h))}}{2\alpha C_n}e^{-k_n|x|},\,\,\,(1)&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
C_n=\frac{1}{2}\left(h + \frac{(5\beta k_n ^4 + 1 - \alpha\gamma)\sin^2{(k_n h)}}{\alpha}\right),&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
and &amp;lt;math&amp;gt;k_n&amp;lt;/math&amp;gt; are the solutions of the [[Dispersion Relation for a Floating Elastic Plate]].  &lt;br /&gt;
&lt;br /&gt;
Consequently, the source functions for a single crack at &amp;lt;math&amp;gt;x=0&amp;lt;/math&amp;gt; can be defined as&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
\psi_s(x,z)= \beta\chi_{xx}(x,z),\,\,\,&lt;br /&gt;
\psi_a(x,z)= \beta\chi_{xxx}(x,z),\,\,\,(2)&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
It can easily be shown that &amp;lt;math&amp;gt;\psi_s&amp;lt;/math&amp;gt; is symmetric about &amp;lt;math&amp;gt;x = 0&amp;lt;/math&amp;gt; and &lt;br /&gt;
&amp;lt;math&amp;gt;\psi_a&amp;lt;/math&amp;gt; is antisymmetric about &amp;lt;math&amp;gt;x = 0&amp;lt;/math&amp;gt;.&lt;br /&gt;
&lt;br /&gt;
Substituting (1) into (2) gives&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
\psi_s(x,z)= &lt;br /&gt;
{&lt;br /&gt;
-\frac{\beta}{\alpha}&lt;br /&gt;
\sum_{n=-2}^\infty &lt;br /&gt;
\frac{g_n\cos{(k_n(z+h))}}{2k_{xn}C_n}e^{k_n|x|} },&lt;br /&gt;
\psi_a(x,z)= &lt;br /&gt;
{&lt;br /&gt;
{\rm sgn}(x) i\frac{\beta}{\alpha}\sum_{n=-2}^\infty &lt;br /&gt;
\frac{g_n&#039;\cos{(k_n(z+h))}}{2k_{xn}C_n}e^{k_n|x|}},&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
g_n = ik_n^3 \sin{k_n h},\,\,\,\,&lt;br /&gt;
g&#039;_n= -k_n^4 \sin{k_n h}.&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
We then express the solution to the problem as a linear combination of the &lt;br /&gt;
incident wave and pairs of source functions at each crack,&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
\phi(x,z) = &lt;br /&gt;
e^{-k_0 x}\frac{\cos(k_0(z+h))}{\cos(k_0h)}&lt;br /&gt;
+ (P\psi_s(x,z) + Q\psi_a(x,z))\,\,\,(3)&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where &amp;lt;math&amp;gt;P&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;Q&amp;lt;/math&amp;gt; are coefficients to be solved which represent the jump in the gradient &lt;br /&gt;
and elevation respectively of the plates across the crack &amp;lt;math&amp;gt;x = a_j&amp;lt;/math&amp;gt;. &lt;br /&gt;
The coefficients &amp;lt;math&amp;gt;P&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;Q&amp;lt;/math&amp;gt; are found by applying the edge conditions  and to&lt;br /&gt;
the &amp;lt;math&amp;gt;z&amp;lt;/math&amp;gt; derivative of &amp;lt;math&amp;gt;\phi&amp;lt;/math&amp;gt; at &amp;lt;math&amp;gt;z=0&amp;lt;/math&amp;gt;,&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
\frac{\partial^2}{\partial x^2}\left. \frac{\partial \phi}{\partial z}\right|_{x=0,z=0}=0,\,\,\,&lt;br /&gt;
{\rm and}\,\,\,\,&lt;br /&gt;
\frac{\partial^3}{\partial x^3}\left. \frac{\partial \phi}{\partial z}\right|_{x=0,z=0}=0.&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
The reflection and transmission coefficients, &amp;lt;math&amp;gt;R&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;T&amp;lt;/math&amp;gt; can be found from (3) &lt;br /&gt;
by taking the limits as &amp;lt;math&amp;gt;x\rightarrow\pm\infty&amp;lt;/math&amp;gt; to obtain&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt; &lt;br /&gt;
R = {- \frac{\beta}{\alpha}&lt;br /&gt;
(g&#039;_0Q + ig_0P)}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
and &lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
T= 1 + {\frac{\beta}{\alpha}(g&#039;_0Q - ig_0P)}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
=== Two Semi-Infinite Plates of Different Properties ===&lt;br /&gt;
&lt;br /&gt;
The next most simple problem is two semi-infinite plates of different properties. Often one of&lt;br /&gt;
the plates is taken to be open water which makes the problem simpler. In general, the solution method&lt;br /&gt;
developed for open water can be extended to two plates of different properties, the exception to&lt;br /&gt;
this is the [[Residue Calculus]] solution which applies only when one of the semi-infinite regions&lt;br /&gt;
is water.&lt;br /&gt;
&lt;br /&gt;
====[[Wiener-Hopf]]====&lt;br /&gt;
&lt;br /&gt;
The solution to the problem of two semi-infinite plates with different properties can be&lt;br /&gt;
solved by the Wiener-Hopf method. The first work on this problem was by [[Evans and Davies 1968]] &lt;br /&gt;
but they did not actually develop the method sufficiently to be able to calculate the solution.&lt;br /&gt;
The explicit solution was not found until the work of ...&lt;br /&gt;
&lt;br /&gt;
====[[Eigenfunction Matching Method]]====&lt;br /&gt;
&lt;br /&gt;
The eigenfunction matching solution was developed by [[Fox and Squire 1994]].&lt;br /&gt;
Essentially the solution is expanded on either side of the crack.&lt;br /&gt;
&lt;br /&gt;
====[[Residue Calculus]]====&lt;br /&gt;
&lt;br /&gt;
= Three Dimensional Problem =&lt;br /&gt;
&lt;br /&gt;
== Equations of Motion == &lt;br /&gt;
&lt;br /&gt;
For a classical thin plate, the equation of motion is given by &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
D\nabla ^4 w + \rho _i h w = p&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
Equation ((plate)) is subject to the free edge boundary&lt;br /&gt;
conditions for a thin plate &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\frac{\partial ^{2}w}{\partial n^{2}}+\nu \frac{\partial ^{2}w}{\partial&lt;br /&gt;
s^{2}}=0,\;\;\;=\textrm{and= }\mathrm{\;\;\;}\frac{\partial ^{3}w}{&lt;br /&gt;
\partial n^{3}}+\left( 2-\nu \right) \frac{\partial ^{3}w}{\partial&lt;br /&gt;
n\partial s^{2}}=0,&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
[[Hildebrand65]] where &amp;lt;math&amp;gt;n&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;s&amp;lt;/math&amp;gt; denote the normal and tangential&lt;br /&gt;
directions respectively.&lt;br /&gt;
&lt;br /&gt;
The pressure, &amp;lt;math&amp;gt;p&amp;lt;/math&amp;gt;, is given by the linearized Bernoulli&#039;s equation at the&lt;br /&gt;
water surface, &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
p=-\rho \frac{\partial \phi }{\partial t}-\rho gW &lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
where &amp;lt;math&amp;gt;\Phi &amp;lt;/math&amp;gt; is the velocity potential of the water, &amp;lt;math&amp;gt;\rho &amp;lt;/math&amp;gt; is the density&lt;br /&gt;
of the water, and &amp;lt;math&amp;gt;g&amp;lt;/math&amp;gt; is the acceleration due to gravity.&lt;br /&gt;
&lt;br /&gt;
We now introduce non-dimensional variables. We non-dimensionalise the length&lt;br /&gt;
variables with respect to &amp;lt;math&amp;gt;a&amp;lt;/math&amp;gt; where the surface area of the floe is &amp;lt;math&amp;gt;4a^{2}.&amp;lt;/math&amp;gt;&lt;br /&gt;
We non-dimensionalise the time variables with respect to &amp;lt;math&amp;gt;\sqrt{g/a}&amp;lt;/math&amp;gt; and&lt;br /&gt;
the mass variables with respect to &amp;lt;math&amp;gt;\rho a^{3}&amp;lt;/math&amp;gt;. &lt;br /&gt;
In the non-dimensional variables equations ((plate)) and ((pressure)&lt;br /&gt;
) become &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\beta \nabla ^{4}\bar{w}+\gamma \frac{\partial ^{2}\bar{w}}{\partial \bar{t}&lt;br /&gt;
^{2}}=\frac{\partial \bar{\Phi}}{\partial \bar{t}}-\bar{w},   (n-d_ice)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
where &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\beta =\frac{D}{g\rho a^{4}}, \; \mathbf{and} \; \gamma =\frac{\rho _{i}h}{\rho&lt;br /&gt;
a}. &lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
We shall refer to &amp;lt;math&amp;gt;\beta &amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;\gamma &amp;lt;/math&amp;gt; as the stiffness and mass&lt;br /&gt;
respectively.&lt;br /&gt;
&lt;br /&gt;
We will determine the response of the ice floe to wave forcing of a single&lt;br /&gt;
frequency (the response for more complex wave forcing can be found by&lt;br /&gt;
superposition of the single frequency solutions). Since the equations of&lt;br /&gt;
motion are linear the displacement and potential must have the same single&lt;br /&gt;
frequency dependence. Therefore they can be expressed as the real part of a&lt;br /&gt;
complex quantity whose time dependence is &amp;lt;math&amp;gt;e^{-i\sqrt{\alpha }t}&amp;lt;/math&amp;gt; where &amp;lt;math&amp;gt;&lt;br /&gt;
\alpha &amp;lt;/math&amp;gt; is the non-dimensional wavenumber and we write &amp;lt;math&amp;gt;\bar{W}(\bar{x},&lt;br /&gt;
\bar{y},\bar{t})={Re}\left[ w\left( \bar{x},\bar{y}\right) e^{-i\sqrt{&lt;br /&gt;
\alpha }\bar{t}}\right] \ &amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;\;\Phi (\bar{x},\bar{y},\bar{z},\bar{t})=&lt;br /&gt;
{Re}\left[ \phi \left( \bar{x},\bar{y},\bar{z}\right) e^{-i\sqrt{\alpha &lt;br /&gt;
}\bar{t}}\right] .&amp;lt;/math&amp;gt; In the complex variables the equation of motion of the&lt;br /&gt;
ice floe ((n-d_ice)) is &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\beta \nabla ^{4}w+\alpha \gamma w=\sqrt{\alpha }\phi -w.   (plate2)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
From now on we will drop the overbar and assume all variables are&lt;br /&gt;
non-dimensional.&lt;br /&gt;
&lt;br /&gt;
==Equations of Motion for the Water==&lt;br /&gt;
&lt;br /&gt;
We require the equation of motion for the water to solve equation (\ref&lt;br /&gt;
{plate2}). We begin with the non-dimensional equations of potential theory&lt;br /&gt;
which describe linear surface gravity waves &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;   (bvp)&lt;br /&gt;
\left. &lt;br /&gt;
\begin{matrix}{rr}&lt;br /&gt;
\nabla ^{2}\phi =0, &amp;amp; -\infty &amp;lt;z&amp;lt;0, \\ &lt;br /&gt;
{\frac{\partial \phi }{\partial z}=0}, &amp;amp; z\rightarrow -\infty , \\ &lt;br /&gt;
{\frac{\partial \phi }{\partial z}=}-i\sqrt{\alpha }w, &amp;amp; z\;=\;0,\;\;&lt;br /&gt;
\mathbf{x}\in \Delta , \\ &lt;br /&gt;
{\frac{\partial \phi }{\partial z}-}\alpha \phi {=}p, &amp;amp; z\;=\;0,\;\;\mathbf{&lt;br /&gt;
x}\notin \Delta ,&lt;br /&gt;
\end{matrix}&lt;br /&gt;
\right\}    (bvp_nond)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
([[Weh_Lait]]). As before, &amp;lt;math&amp;gt;w&amp;lt;/math&amp;gt; is the displacement of the floe and &amp;lt;math&amp;gt;p&amp;lt;/math&amp;gt;&lt;br /&gt;
is the pressure at the water surface. The vector &amp;lt;math&amp;gt;\mathbf{x=(}x,y)&amp;lt;/math&amp;gt; is a&lt;br /&gt;
point on the water surface and &amp;lt;math&amp;gt;\Delta &amp;lt;/math&amp;gt; is the region of the water surface&lt;br /&gt;
occupied by the floe. The water is assumed infinitely deep. A schematic&lt;br /&gt;
diagram of this problem is shown in Figure (vibration). &lt;br /&gt;
\begin{figure}[tbp]&lt;br /&gt;
\begin{center}&lt;br /&gt;
\epsfbox{vibration.eps}&lt;br /&gt;
\end{center}&lt;br /&gt;
\caption{{The schematic diagram of the boundary value problem and the&lt;br /&gt;
coordinate system used in the solution.}}&lt;br /&gt;
 (vibration)&lt;br /&gt;
\end{figure}&lt;br /&gt;
&lt;br /&gt;
The boundary value problem ((bvp)) is subject to an incident wave which&lt;br /&gt;
is imposed through a boundary condition as &amp;lt;math&amp;gt;\left| \mathbf{x}\right|&lt;br /&gt;
\rightarrow \infty &amp;lt;/math&amp;gt;. This boundary condition, which is called the&lt;br /&gt;
Sommerfeld radiation condition, is essentially that at large distances the&lt;br /&gt;
potential consists of a radial outgoing wave (the wave generated by the ice&lt;br /&gt;
floe motion) and the incident wave. It is expressed mathematically as &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\lim_{\left| \mathbf{x}\right| \rightarrow \infty }\sqrt{|\mathbf{x}|}\left( &lt;br /&gt;
\frac{\partial }{\partial |\mathbf{x}|}-i\alpha \right) (\phi -\phi ^{&lt;br /&gt;
\mathrm{In}})=0,   (summerfield)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
[[Weh_Lait]]. The incident potential (i.e. the incoming wave) &amp;lt;math&amp;gt;\phi ^{&lt;br /&gt;
\mathrm{In}}&amp;lt;/math&amp;gt; is &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\phi ^{\mathrm{In}}(x,y,z)=\frac{A}{\sqrt{\alpha }}e^{i\alpha (x\cos \theta&lt;br /&gt;
+y\sin \theta )}e^{\alpha z},   (input)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
where &amp;lt;math&amp;gt;A&amp;lt;/math&amp;gt; is the non-dimensional wave amplitude.&lt;br /&gt;
&lt;br /&gt;
The standard solution method to the linear wave problem is to transform the&lt;br /&gt;
boundary value problem into an integral equation using a Green function &lt;br /&gt;
\citep{john1,&lt;br /&gt;
john2,Sarp_Isa,jgrfloecirc}. Performing such a transformation, the boundary&lt;br /&gt;
value problem ((bvp)) and ((summerfield)) becomes &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\phi (\mathbf{x})=\phi ^{i}(\mathbf{x})+\iint_{\Delta }G_{\alpha }(\mathbf{x}&lt;br /&gt;
;\mathbf{y})\left( \alpha \phi (\mathbf{x})+i\sqrt{\alpha }w(\mathbf{x}&lt;br /&gt;
)\right) dS_{\mathbf{y}}.   (water)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
The Green function &amp;lt;math&amp;gt;G_{\alpha }&amp;lt;/math&amp;gt; is &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
G_{\alpha }(\mathbf{x};\mathbf{y)}=\frac{1}{4\pi }\left( \frac{2}{|\mathbf{x}&lt;br /&gt;
-\mathbf{y}|}-\pi \alpha \left( \mathbf{H_{0}}(\alpha |\mathbf{x}-\mathbf{y}&lt;br /&gt;
|)+Y_{0}(\alpha |\mathbf{x}-\mathbf{y}|)\right) +2\pi i\alpha J_{0}(\alpha |&lt;br /&gt;
\mathbf{x}-\mathbf{y}|)\right) , &lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
[[Weh_Lait,jgrfloecirc]], where &amp;lt;math&amp;gt;J_{0}&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;Y_{0}&amp;lt;/math&amp;gt; are respectively&lt;br /&gt;
Bessel functions of the first and second kind of order zero, and &amp;lt;math&amp;gt;\mathbf{&lt;br /&gt;
H_{0}}&amp;lt;/math&amp;gt; is the Struve function of order zero [[abr_ste]]. A solution for&lt;br /&gt;
water of finite depth could be found by simply using the depth dependent&lt;br /&gt;
Green function [[Weh_Lait]].&lt;br /&gt;
&lt;br /&gt;
The integral equation ((water)) will be solved using numerical&lt;br /&gt;
integration. The only difficulty arises from the non-trivial nature of the&lt;br /&gt;
kernel of the integral equation (the Green function). However, the Green&lt;br /&gt;
function has no &amp;lt;math&amp;gt;z&amp;lt;/math&amp;gt; dependence due to the shallow draft approximation and&lt;br /&gt;
depends only on &amp;lt;math&amp;gt;|\mathbf{x}-\mathbf{y}|.&amp;lt;/math&amp;gt; This means that the Green&lt;br /&gt;
function is one dimensional and the values which are required for a given&lt;br /&gt;
calculation can be looked up in a previously computed table.&lt;br /&gt;
&lt;br /&gt;
==Solving for the Wave Induced Ice Floe Motion==&lt;br /&gt;
&lt;br /&gt;
To determine the ice floe motion we must solve equations ((plate2)) and (&lt;br /&gt;
(water)) simultaneously. We do this by expanding the floe motion in the&lt;br /&gt;
free modes of vibration of a thin plate. The major difficulty with this&lt;br /&gt;
method is that the free modes of vibration can be determined analytically&lt;br /&gt;
only for very restrictive geometries, e.g. a circular thin plate. Even the&lt;br /&gt;
free modes of vibration of a square plate with free edges must be determined&lt;br /&gt;
numerically. This is the reason why the solution of [[jgrfloecirc]] was&lt;br /&gt;
only for a circular floe.&lt;br /&gt;
&lt;br /&gt;
Since the operator &amp;lt;math&amp;gt;\nabla ^{4},&amp;lt;/math&amp;gt; subject to the free edge boundary&lt;br /&gt;
conditions, is self adjoint a thin plate must possess a set of modes &amp;lt;math&amp;gt;w_{i}&amp;lt;/math&amp;gt;&lt;br /&gt;
which satisfy the free boundary conditions and the following eigenvalue&lt;br /&gt;
equation &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\nabla ^{4}w_{i}=\lambda _{i}w_{i}. &lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
The modes which correspond to different eigenvalues &amp;lt;math&amp;gt;\lambda _{i}&amp;lt;/math&amp;gt; are&lt;br /&gt;
orthogonal and the eigenvalues are positive and real. While the plate will&lt;br /&gt;
always have repeated eigenvalues, orthogonal modes can still be found and&lt;br /&gt;
the modes can be normalized. We therefore assume that the modes are&lt;br /&gt;
orthonormal, i.e. &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\iint_{\Delta }w_{i}\left( \mathbf{Q}\right) w_{j}\left( \mathbf{Q}\right)&lt;br /&gt;
dS_{\mathbf{Q}}=\delta _{ij} &lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
where &amp;lt;math&amp;gt;\delta _{ij}&amp;lt;/math&amp;gt; is the Kronecker delta. The eigenvalues &amp;lt;math&amp;gt;\lambda _{i}&amp;lt;/math&amp;gt;&lt;br /&gt;
have the property that &amp;lt;math&amp;gt;\lambda _{i}\rightarrow \infty &amp;lt;/math&amp;gt; as &amp;lt;math&amp;gt;i\rightarrow&lt;br /&gt;
\infty &amp;lt;/math&amp;gt; and we order the modes by increasing eigenvalue. These modes can be&lt;br /&gt;
used to expand any function over the wetted surface of the ice floe &amp;lt;math&amp;gt;\Delta &amp;lt;/math&amp;gt;&lt;br /&gt;
.&lt;br /&gt;
&lt;br /&gt;
We expand the displacement of the floe in a finite number of modes &amp;lt;math&amp;gt;N,&amp;lt;/math&amp;gt; i.e. &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
w\left( \mathbf{x}\right) =\sum_{i=1}^{N}c_{i}w_{i}\left( \mathbf{x}\right) .&lt;br /&gt;
 (expansion)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
From the linearity of ((water)) the potential can be written in the&lt;br /&gt;
following form &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\phi =\phi _{0}+\sum_{i=1}^{N}c_{i}\phi _{i}   (expansionphi)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
where &amp;lt;math&amp;gt;\phi _{0}&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;\phi _{i}&amp;lt;/math&amp;gt; satisfy the integral equations &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\phi _{0}(\mathbf{x})=\phi ^{\mathrm{In}}(\mathbf{x})+\iint_{\Delta }\alpha&lt;br /&gt;
G_{\alpha }(\mathbf{x};\mathbf{y})\phi (\mathbf{y})dS_{\mathbf{y}}&lt;br /&gt;
 (phi0)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
and &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\phi _{i}(\mathbf{x})=\iint_{\Delta }G_{\alpha }(\mathbf{x};\mathbf{y}&lt;br /&gt;
)\left( \alpha \phi _{i}(\mathbf{x})+i\sqrt{\alpha }w_{i}(\mathbf{y})\right)&lt;br /&gt;
dS_{\mathbf{y}}.   (phii)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
The potential &amp;lt;math&amp;gt;\phi _{0}&amp;lt;/math&amp;gt; represents the potential due the incoming wave&lt;br /&gt;
assuming that the displacement of the ice floe is zero. The potentials &amp;lt;math&amp;gt;\phi&lt;br /&gt;
_{i}&amp;lt;/math&amp;gt; represent the potential which is generated by the plate vibrating with&lt;br /&gt;
the &amp;lt;math&amp;gt;i&amp;lt;/math&amp;gt;th mode in the absence of any input wave forcing.&lt;br /&gt;
&lt;br /&gt;
We substitute equations ((expansion)) and ((expansionphi)) into&lt;br /&gt;
equation ((plate2)) to obtain &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\beta \sum_{i=1}^{N}\lambda _{i}c_{i}w_{i}-\alpha \gamma&lt;br /&gt;
\sum_{i=1}^{N}c_{i}w_{i}=i\sqrt{\alpha }\left( \phi&lt;br /&gt;
_{0}+\sum_{i=1}^{N}c_{i}\phi _{i}\right) -\sum_{i=1}^{N}c_{i}w_{i}.&lt;br /&gt;
 (expanded)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
To solve equation ((expanded)) we multiply by &amp;lt;math&amp;gt;w_{j}&amp;lt;/math&amp;gt; and integrate over&lt;br /&gt;
the plate (i.e. we take the inner product with respect to &amp;lt;math&amp;gt;w_{j})&amp;lt;/math&amp;gt; taking&lt;br /&gt;
into account the orthogonality of the modes &amp;lt;math&amp;gt;w_{i}&amp;lt;/math&amp;gt;, and obtain &lt;br /&gt;
&amp;lt;center&amp;gt;&amp;lt;math&amp;gt;&lt;br /&gt;
\beta \lambda _{j}c_{j}+\left( 1-\alpha \gamma \right) c_{j}=\iint_{\Delta }i&lt;br /&gt;
\sqrt{\alpha }\left( \phi _{0}\left( \mathbf{Q}\right)&lt;br /&gt;
+\sum_{i=1}^{N}c_{i}\phi _{i}\left( \mathbf{Q}\right) \right) w_{j}\left( &lt;br /&gt;
\mathbf{Q}\right) dS_{\mathbf{Q}}   (final)&lt;br /&gt;
&amp;lt;/math&amp;gt;&amp;lt;/center&amp;gt;&lt;br /&gt;
which is a matrix equation in &amp;lt;math&amp;gt;c_{i}.&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
We cannot solve equation ((final)) without determining the modes of&lt;br /&gt;
vibration of the thin plate &amp;lt;math&amp;gt;w_{i}&amp;lt;/math&amp;gt; (along with the associated eigenvalues &amp;lt;math&amp;gt;&lt;br /&gt;
\lambda _{i})&amp;lt;/math&amp;gt; and solving the integral equations ((phi0)) and (\ref&lt;br /&gt;
{phii}). We use the finite element method to determine the modes of&lt;br /&gt;
vibration [[Zienkiewicz]] and the integral equations ((phi0)) and (&lt;br /&gt;
(phii)) are solved by a constant panel method [[Sarp_Isa]]. The same&lt;br /&gt;
set of nodes is used for the finite element method and to define the panels&lt;br /&gt;
for the integral equation.&lt;br /&gt;
&lt;br /&gt;
[[Category:Linear Hydroelasticity]]&lt;/div&gt;</summary>
		<author><name>Hyuck</name></author>
	</entry>
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