Structural efficiency of orthotropic cylindrical shells subjected toaxial compression.
Author:
Affiliation:
1. General Electric Company, King of Prussia, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3461
Reference11 articles.
1. MINIMUM WEIGHT POTENTIALS FOR STIFFENED PLATES AND SHELLS
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