Table 1.

Honeycomb sandwich panel parameters.

${\mathit{a}}_0\left(\mathbf{m}\mathbf{m}\right)$	${\mathit{b}}_0\left(\mathbf{m}\mathbf{m}\right)$	${\mathit{h}}_{\mathbf{c}}\left(\mathbf{m}\mathbf{m}\right)$	${\mathit{h}}_{\mathbf{f}}\left(\mathbf{m}\mathbf{m}\right)$	${\mathit{E}}_{\mathbf{f}}\left(\mathbf{G}\mathbf{P}\mathbf{a}\right)$
$\mathbf{6}$	$1$	$2$	$1$	$200$
${\mathit{\rho }}_{\mathbf{f}}\left(kg/m^3\right)$	${\rho }_{\mathrm{c}}\left(\mathrm{kg}/{\mathrm{m}}^3\right)$	${\nu }_{\mathrm{f}}$	$a_x$	$a_y$
$\mathbf{8960}$	$8960$	$0.32$	$4\sqrt{3}{a}_0+4b_0$	$6a_0+2\sqrt{3}{b}_0$