Abstract
An analytical solution of the deflection of the sandwich twist specimen based on first-order shear deformation theory is presented. The solution utilizes a Fourier series approach for the loading and displacements. Parametric analysis of the influences of face and core stiffnesses, core thickness and panel in-plane size on the plate compliance is conducted. The results are compared to finite element analysis. The first-order shear deformation compliance results are in good agreement with finite element analysis for sandwich panels with soft, shear deformable cores, whereas for stiff cores the first-order shear deformation solution underpredicts the panel compliance. Reasons for the discrepancy and limits for the use of the analysis are discussed.
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