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Postbuckling response and failure prediction of graphite-epoxy plates loaded in compression

1992; American Institute of Aeronautics and Astronautics; Volume: 30; Issue: 8 Linguagem: Inglês

10.2514/3.11187

1533-385X

Stephen P. Engelstad, J. N. Reddy, N. F. Knight,

Structural Load-Bearing Analysis

A shear deformable (three-dimensional) shell element is used to analyze the panels. Two panels without boles and one with a bole are studied, and the resulting responses and failure modes comelated well with the experimental results.