A study of the buckling of laminated composite plates
Author:
Affiliation:
1. Case Western Reserve University, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6237
Reference24 articles.
1. Minimum Weight Analysis of Orthotropic Plates Under Compressive Loading
2. On the analysis of experimental observations in problems of elastic stability
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