General instability and face wrinkling of sandwich plates - Unified theory and applications.
Author:
Affiliation:
1. Stanford University, Stanford, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4054
Reference30 articles.
1. The Stabilisation of a Thin Sheet by a Continuous Supporting Medium
2. Williams, D., Leggett, D. M. A., and Hopkins, H. G. "Flat sandwich panels under compressive end loads/' Aeronautical Research Council R. & M. 1987 (1941).
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