Formulation of the mathematical problem
The proposed model is composed of two vertically floating identical plates interconnected through hinges by means of two horizontal bars with dampers, see Fig. 3, and allowed to sway and roll. We consider a two-dimensional model in the (x, z) plane. The x-axis coincides with the undisturbed water surface and the z-axis points downwards. We assume irrotational flow in infinitely deep water, and remain within the framework of linear wave theory. Thus, the governing equation and free-surface boundary conditions are
$$\begin{aligned}&\phi _{,xx}+\phi _{,zz}=0, \quad z\ge 0 \end{aligned}$$
(8)
$$\begin{aligned}&\phi _{,\tau \tau }-g\phi _{,z}=0, \quad z=0, \end{aligned}$$
(9)
where \(\phi \) is the velocity potential, \(\tau \) is the time, and the subscripts preceded by a comma denote partial differentiation.
The potential of an incident wave, with frequency \(\omega \), and unit amplitude, approaching from the left (\(x=-\infty \)) is given by
$$\begin{aligned} \phi _{0}=-\frac{jg}{\omega }{\text {exp}}[{j \omega \tau -k(z+jx)}], \end{aligned}$$
(10)
with \(k=\omega ^2/g, \, j=\sqrt{-1}\).
The boundary conditions on the plates (1) and (2) (after linearisation) are
$$\begin{aligned}&\phi _{,x} = j \omega (H_1 + A_1 z), \quad x=0 \text { and } 0 < z < T,\end{aligned}$$
(11)
$$\begin{aligned}&\phi _{,x} = j \omega (H_2 + A_2 z), \quad x = C \text { and } 0 < z < T. \end{aligned}$$
(12)
\(H_1\) and \(H_2\) are the ratios between the horizontal displacement amplitudes of the points (0, 0) and (C, 0) and the incident wave amplitude, respectively. \(A_1\) and \(A_2\) are the amplitudes of the angular motions of the plate about (0, 0) and (C, 0) per unit wave amplitude, respectively.
The solution of the mathematical problem is rendered unique with the help of the so-called radiation conditions at \(x \rightarrow \pm \infty .\)
In Sect. 3.2, we summarize the closed mathematical solution for a single plate as given by Haskind (1959). An experimental verification of Haskind’s solution is given by Stiassnie et al. (1981). In Sect. 3.3, we utilise the wide spacing assumption, see Srokosz and Evans (1979), to obtain a formulation in the form of a linear algebraic system of equations. Section 3.4 contains energy balance considerations.
Haskind’s solution for a single plate
The case of a single plate has been studied by numerous investigators [notably Ursell (1947, 1948), and in the context of floating breakwaters by Stiassnie (1980)]. The following is based on results of Haskind (1959). The transmission coefficient \(T_\mathrm{t}\) (defined as the ratio of transmitted to incident wave amplitude) for a thin plate, submerged to a depth T, is given by
$$\begin{aligned} T_\mathrm{t}=t+B_2H+B_4A, \end{aligned}$$
(13)
where t is the transmission coefficient of a rigidly held plate; H is the ratio between the horizontal displacement amplitude of the point O (intersection between the plate and the undisturbed water surface) and the incident wave amplitude; A is the amplitude of the angular motion about O per unit wave amplitude. For the case of a weightless freely floating plate, the expressions for H and A are:
$$\begin{aligned}&H=(-Y_gD_{44}+M_gD_{24})/D; \end{aligned}$$
(14a)
$$\begin{aligned}&A=(Y_gD_{42}-M_gD_{22})/D. \end{aligned}$$
(14b)
The physical meaning of each of the various quantities in Eqs. (13) and (14) is as follows: \(B_2\), \(B_4\) are the amplitudes of the waves radiated in the positive direction by a unit amplitude of horizontal and angular displacements, respectively, for a single plate; \(Y_g\), \(M_g\) are the force and moment exerted on the plate by a unit amplitude wave arriving from the left. We also have
$$\begin{aligned}&D_{pq}=\omega ^2\mu _{pq}-j\omega \lambda _{pq} \qquad (p \text { and } q=2,4);\end{aligned}$$
(15a)
$$\begin{aligned}&D=D_{22}D_{44}-D_{24}D_{42}, \end{aligned}$$
(15b)
where \(\mu _{pq}\) are the added mass coefficients and \(\lambda _{pq}\) are the damping coefficients. As in Srokosz and Evans’ (1979) treatment of two thin barriers, here too the mass and moment of inertia are negligible compared with the added mass and damping due to the fluid. The indices 2 and 4 refer to horizontal and angular motions, respectively. The detailed mathematical expressions for the above-mentioned quantities are rather long and are given in Appendix 1.
Solution for twin plates
The wide spacing assumption means that the plates are spaced far enough from one another, so that the local wave field in the vicinity of one plate (i.e., the evanescent part) does not influence the other. The only interaction between the plates is due to the far field propagating wave terms which appear in the radiation and scattering problems for a single plate. Let us observe now two identical plates as shown in Fig. 4. The terms \(R_1\), \(R_2\) denote the amplitudes of the waves traveling to the right. The amplitudes of the waves traveling to the left are denoted by \(L_1\), \(L_2\). The subscript \(i=1,2\) indicates that the wave approaches the ith plate (either from its right or left side). Without loss of generality the incident wave from the left was considered to have a unit amplitude, i.e., \(R_1=1\). The parameter \(L_2\) was set equal to zero in accordance with Sommerfeld’s radiation condition. As mentioned in Sect. 2.1, we denote the horizontal displacements of the intersection points of the plates \(i=1,2\) and the undisturbed water surface by \(H_1\), \(H_2\). The quantities \(A_1\), \(A_2\) are the amplitudes of the angular motion about these intersection points.
\(H_1\), \(H_2\), \(A_1\), \(A_2\), \(R_2\), and \(L_1\) constitute the six unknown variables of the problem, whereas \(\omega \), T, C, and d are given parameters. Neglecting the mass of the plates reduces their equations of horizontal/angular motion to balances of forces/moments. The balances of horizontal forces, for plates 1, 2, respectively, gives
$$\begin{aligned}&D_{22}H_1+D_{24}A_1+Y_g(R_1-L_1)-2j\omega d(H_1-H_2) \nonumber \\&\quad -j\omega T d (A_1-A_2)=0, \end{aligned}$$
(16)
$$\begin{aligned}&D_{22}H_2+D_{24}A_2+Y_gR_2+2j\omega d(H_1-H_2)\nonumber \\&\quad +j\omega T d (A_1-A_2)=0. \end{aligned}$$
(17)
The balances of moments, for plates 1, 2 are, respectively,
$$\begin{aligned}&D_{24}H_1+D_{44}A_1+M_g(R_1-L_1)-j\omega Td(H_1-H_2)\nonumber \\&\quad -j\omega T^2 d (A_1-A_2)=0,\end{aligned}$$
(18)
$$\begin{aligned}&D_{24}H_2+D_{44}A_2+M_gR_2+j\omega Td(H_1-H_2)\nonumber \\&\quad +j\omega T^2 d (A_1-A_2)=0. \end{aligned}$$
(19)
A consequence of the wide spacing assumption is that the far field to the right of plate 1 is identical with the far field to the left of plate 2. In this way we obtain an additional pair of equations, one for the wave propagating in the positive direction and the other for the wave propagating in the negative direction:
$$\begin{aligned}&B_2H_1+B_4A_1+tR_1+rL_1=ER_2,\end{aligned}$$
(20)
$$\begin{aligned}&-B_2H_2-B_4A_2+rR_2=EL_1, \end{aligned}$$
(21)
where r is the reflection coefficient for a rigidly held single plate and \(E=exp(jkC)\). Equations (16)–(21) constitute together a linear algebraic system of six equations with the same number of unknowns.
Energy balance
Neglecting energy dissipation due to vortex shedding from the lower edges of the plates (see Stiassnie et al. 1984), the (time averaged) incoming energy flux, \(F_\mathrm{i}\), should equal the sum of the reflected energy flux \(F_\mathrm{r}\), the transmitted energy flux \(F_\mathrm{t}\), and the power absorbed by the dampers \(P_\mathrm{a}\):
$$\begin{aligned} F_\mathrm{i}=F_\mathrm{r}+F_\mathrm{t}+P_\mathrm{a}. \end{aligned}$$
(22)
The fluxes are given by multiplying the energy densities by the group velocity \(c_g=0.5\omega /k\); which gives, for \(R_1=1\),
$$\begin{aligned}&F_\mathrm{i}=\left( \frac{1}{2}\rho g\right) c_g, \end{aligned}$$
(23)
$$\begin{aligned}&F_\mathrm{r}=\left( \frac{1}{2}\rho g\right) |T_\mathrm{r}^2|c_g, \end{aligned}$$
(24)
$$\begin{aligned}&\text {and}\nonumber \\&F_\mathrm{t}=\left( \frac{1}{2}\rho g\right) |T_\mathrm{t}^2|c_g, \end{aligned}$$
(25)
where the reflection coefficient, \(T_\mathrm{r}\), and transmission coefficient, \(T_\mathrm{t}\), for the two-plate system, are
$$\begin{aligned}&T_\mathrm{r}=r-B_2H_1-B_4A_1+tL_1,\end{aligned}$$
(26)
$$\begin{aligned}&T_\mathrm{t}=tR_2+B_2H_2+B_4A_2. \end{aligned}$$
(27)
The time averaged power that is absorbed by both dampers is
$$\begin{aligned} P_\mathrm{a}=\frac{1}{2}\rho \omega ^2d(|H_1-H_2|^2+|H_1+TA_1-H_2-TA_2|^2).\nonumber \\ \end{aligned}$$
(28)
Note that the relative error in our calculations, given by
$$\begin{aligned} er=|F_\mathrm{i}-F_\mathrm{r}-F_\mathrm{t}-P_\mathrm{a}|/F_\mathrm{i}, \end{aligned}$$
(29)
was always found to be less than \(10^{-4}\).
We find a maximum value for dimensionless absorbed power \(P_\mathrm{a}/F_\mathrm{i}\) [see (28)] of 0.5 for nondimensional draft \(T_m = 0.71 k_\mathrm{p}^{-1},\) plate spacing \(C_m = 1.05 k_\mathrm{p}^{-1},\) and damping \(d_m = 0.88 g^{1/2} k_\mathrm{p}^{-3/2},\) where \(k_\mathrm{p}\) is the wavenumber to which the system is tuned. This chosen maximum is not unique—further details are given in Appendix 2. Note also that this is smaller than what can be attained by a link with a fixed mechanical reference (such as the ground), where a maximum for dimensionless absorbed power of 1 is possible.