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Sensitivity of buckling loads of anisotropic shells of revolution to geometric imperfections and design changes
Authors:Gerald A. Cohen and Raphael T. Haftka
Affiliation:

Structures Research Associates, Laguna Beach, CA 92651, U.S.A.

Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061, U.S.A

Abstract:Buckling load sensitivity calculations in the shell-of-revolution program FASOR are discussed. This development is based on Koiter's initial postbuckling theory, which has been generalized to include the effect of stiffness changes, as well as geometric imperfections. The implementation in FASOR is valid for anisotropic, as well as orthotropic, shells. Examples are presented for cylindrical panels under axial compression, complete cylindrical shells in torsion, and antisymmetric angle-ply cylindrical panels under edge shear.
Keywords:
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