Under the basic assumptions of material continuity and small elastic deformation and obeying deformation coordination
sandwich panel being subjected to bending and torsion
and foam core subjected to shearing
the equivalent elastic constants of the foam-corrugated composite sandwich structure are derived and the corresponding two-dimensional finite element equivalent model and three-dimensional solid model are established. A comparison between the modal experiment of foam-corrugated composite sandwich beam and finite element calculation indicates the correctness of the deduced equivalent elastic constants. The influence of several key geometrical parameters of the foam-corrugated composite sandwich structure on the natural vibration performance is further discussed. It is found that with the increasing panel thickness
the natural frequency heightens; with the increasing thickness of corrugated ribs
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