Finite-element postbuckling analysis of thin elastic plates
Author:
Affiliation:
1. University of Alberta, Edmonton, Alberta, Canada
2. University of California, Berkeley, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5481
Reference24 articles.
1. NUMERICAL ANALYSIS OF UNSYMMETRICAL BENDING OF SHELLS OF REVOLUTION
2. Analysis of Shells of Revolution Subjected to Symmetrical and Nonsymmetrical Loads
3. Computer analysis of asymmetrical deformation of orthotropic shells of revolution
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