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Nonlinear Dynamic Finite Element Analysis of Thick Transversly Flexible Sandwich Panel on Elastic Foundation with Account of Damage Progression in Time. Part 1. Three-Dimensional Formulation and Two-Dimensional Plate Theory
Authors:V. Y. Perel
Affiliation:(1) Air Force Institute of Technology, Department of Aeronautics and Astronautics, Wright Patterson Air Force Base, Ohio, USA
Abstract:In order to construct a plate theory for a thick transversely compressible sandwich plate with composite laminated face sheets, the author makes simplifying assumptions regarding distribution of transverse strain components in the thickness direction. It is assumed that the transverse strains, i.e., epsixz, epsiyz, and epsizzdo not vary in the thickness direction within the face sheets and the core, but can be different functions of the in-plane coordinates in different sublaminates (the face sheets and the core). An algorithm, which takes account of damage progression in dynamic problems, is incorporated into the computational scheme based on the geometrically nonlinear formulation, and is applied to failure analysis of a sandwich plate under ground impact.__________Translated from Problemy Prochnosti, No. 2, pp. 92 – 106, March – April, 2005
Keywords:transversely flexible sandwich panels  elastic foundation  nonlinear dynamics  damage progression  3D stress state
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