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with $\mathbf{U}^N = (u^N, v^N, w^N)^T$. Simple computations give

0=R1zLα(t,x,y)UNdz=hαt+xzα1/2zα+1/2udz+yzα1/2zα+1/2vdzGα+1/2+Gα1/2,0 = \int_{\mathbb{R}} \mathbf{1}_{z \in L_\alpha(t,x,y)} \nabla \cdot \mathbf{U}^N dz = \frac{\partial h_\alpha}{\partial t} + \frac{\partial}{\partial x} \int_{z_{\alpha-1/2}}^{z_{\alpha+1/2}} u \, dz + \frac{\partial}{\partial y} \int_{z_{\alpha-1/2}}^{z_{\alpha+1/2}} v \, dz - G_{\alpha+1/2} + G_{\alpha-1/2},

leading to

hαt+x,y(hαuα)=Gα+1/2Gα1/2,(28)\frac{\partial h_{\alpha}}{\partial t} + \nabla_{x,y} (h_{\alpha} \mathbf{u}_{\alpha}) = G_{\alpha+1/2} - G_{\alpha-1/2}, \quad (28)

with $G_{\alpha \pm 1/2}$ defined by

Gα+1/2=zα+1/2t+uα+1/2x,yzα+1/2wα+1/2.G_{\alpha+1/2} = \frac{\partial z_{\alpha+1/2}}{\partial t} + \mathbf{u}_{\alpha+1/2} \cdot \nabla_{x,y} z_{\alpha+1/2} - w_{\alpha+1/2}.

The sum for $\alpha = 1, \dots, N$ of the above relations gives Eq. (18) where the kinematic boundary conditions (4), (5) corresponding to

G1/2=GN+1/2=0,(29)G_{1/2} = G_{N+1/2} = 0, \quad (29)

have been used. Similarly, the sum for $j = 1, \dots, \alpha$ of the relations (28) with (29) gives the expression (20) for $G_{\alpha+1/2}$.

Now we consider the Galerkin approximation of Eq. (13) i.e. the quantity

R1zLα(t,x,y)(uNt+x,y(uNuN)+uNwNz+gx,yη)dz=0,\int_{\mathbb{R}} \mathbf{1}_{z \in L_\alpha(t,x,y)} \left( \frac{\partial \mathbf{u}^N}{\partial t} + \nabla_{x,y} (\mathbf{u}^N \otimes \mathbf{u}^N) + \frac{\partial \mathbf{u}^N w^N}{\partial z} + g \nabla_{x,y} \eta \right) dz = 0,

leading, after simple computations, to Eq. (19). $\blacksquare$

Proof of prop. 3.2 In order to obtain (22) we multiply (28) by $g(h+z_b)$ ($|\mathbf{u}_\alpha|^2/2$ and (19) by $\mathbf{u}_\alpha$ then we perform simple manipulations. More precisely, the momentum equation along the x axis multiplied by $u_\alpha$ gives

(t(hαuα)+x(hαuα2+g2hhα)+y(hαuαvα))uα=(ghαzbx+uα+1/2Gα+1/2uα1/2Gα1/2)uα.\left(\frac{\partial}{\partial t}(h_\alpha u_\alpha) + \frac{\partial}{\partial x}\left(h_\alpha u_\alpha^2 + \frac{g}{2}hh_\alpha\right) + \frac{\partial}{\partial y}(h_\alpha u_\alpha v_\alpha)\right)u_\alpha = \\ \left(-gh_\alpha \frac{\partial z_b}{\partial x} + u_{\alpha+1/2}G_{\alpha+1/2} - u_{\alpha-1/2}G_{\alpha-1/2}\right)u_\alpha.

Considering first the left hand side of the preceding equation excluding the pressure terms, we denote

Iu,α=(t(hαuα)+x(hαuα2)+y(hαuαvα))uα,I_{u,\alpha} = \left( \frac{\partial}{\partial t}(h_\alpha u_\alpha) + \frac{\partial}{\partial x}(h_\alpha u_\alpha^2) + \frac{\partial}{\partial y}(h_\alpha u_\alpha v_\alpha) \right) u_\alpha,

and using (28) we have

Iu,α=t(hαuα22)+x(uαhαuα22)+y(vαhαuα22)+uα22(hαt+x,y(hαuα)).I_{u,\alpha} = \frac{\partial}{\partial t} \left( \frac{h_\alpha u_\alpha^2}{2} \right) + \frac{\partial}{\partial x} \left( u_\alpha \frac{h_\alpha u_\alpha^2}{2} \right) + \frac{\partial}{\partial y} \left( v_\alpha \frac{h_\alpha u_\alpha^2}{2} \right) + \frac{u_\alpha^2}{2} \left( \frac{\partial h_\alpha}{\partial t} + \nabla_{x,y} (h_\alpha \mathbf{u}_\alpha) \right).

Now we consider the contribution of the pressure terms over the energy balance i.e.

Ip,u,α=(x(g2hhα)+ghαzbx)uα,I_{p,u,\alpha} = \left( \frac{\partial}{\partial x} \left( \frac{g}{2} hh_{\alpha} \right) + gh_{\alpha} \frac{\partial z_{b}}{\partial x} \right) u_{\alpha},

and it comes

Ip,u,α=ghαx(h+zb)uα=gx(hα(h+zb)uα)g(h+zb)x(hαuα)=x((g2hαh+g2hα(h+2zb))uα)g(h+zb)x(hαuα). \begin{align*} I_{p,u,\alpha} &= gh_{\alpha} \frac{\partial}{\partial x}(h+z_b)u_{\alpha} = g \frac{\partial}{\partial x}(h_{\alpha}(h+z_b)u_{\alpha}) - g(h+z_b) \frac{\partial}{\partial x}(h_{\alpha}u_{\alpha}) \\ &= \frac{\partial}{\partial x}\left(\left(\frac{g}{2}h_{\alpha}h + \frac{g}{2}h_{\alpha}(h+2z_b)\right)u_{\alpha}\right) - g(h+z_b)\frac{\partial}{\partial x}(h_{\alpha}u_{\alpha}). \end{align*}

Performing the same manipulations over the momentum equation along $y$ and adding the terms $I_{u,\alpha}, I_{v,\alpha}, I_{p,u,\alpha}, I_{p,v,\alpha}$ and (28) multiplied by $g(h+z_b)-|\mathbf{u}_\alpha|^2/2$ gives the result. $\blacksquare$