Stability analysis of shells of revolution by the finite-element method.
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4502
Reference26 articles.
1. Large Deflections of Structures Subjected to Heating and External Loads
2. Consistent matrix formulations for structural analysis using finite-element techniques.
3. A discrete element procedure for thin-shell instability analysis.
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