Abstract:A semi-analytical solution was proposed for the free vibration of doubly-curved honeycomb shell with elastic foundation. The kinematics and kinetics of the shell was obtained based on the first-order shear deformation theory and the modified Gibson’s formula. The governing equations for the free vibration of the shell were derived using the Hamilton’s principle with a modified shear correction factor, and solved by a modified Ritz’s method. Numerical results show the accuracy and efficiency of the proposed method. Parametric studies indicate that the trend of natural frequencies versus the thickness ratio is dependent on the stiffness of the elastic foundation, the natural frequencies decrease as the cell wall thickness increases, and fluctuate with the change of the cell angle and lamination angle of the honeycomb structure.
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