Dynamic Buckling of a Rectangular Orthotropic Plate
Author:
Affiliation:
1. The University of Nebraska-Lincoln, Lincoln, Nebr.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50665
Reference11 articles.
1. DYNAMIC BUCKLING OF ELASTIC STRUCTURES: CRITERIA AND ESTIMATES**This work was supported in part by the National Aeronautics and Space Administration under Grant NsG-559, and by the Division of Engineering and Applied Physics, Harvard University
2. Buckling of Anisotropic Composite Plates
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