Finite Element Modeling of the Buckling Response of Sandwich Panels
Author:
Affiliation:
1. NASA Langley Research Center
2. Lockheed-Martin Engineering and Sciences Company
3. Veridian Systems Division
4. Lockheed-Martin Advanced Technology Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1517
Reference30 articles.
1. Plantema, F. J., Sandwich Construction, John Wiley,NewYork,1966.
2. General instability and face wrinkling of sandwich plates - Unified theory and applications.
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