Dynamic Snap-Through of Thin-Walled Structures by a Reduced-Order Method
Author:
Affiliation:
1. National Institute of Aerospace, Hampton, Virginia 23666
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.26351
Reference26 articles.
1. Experimental snap-through boundaries for acoustically excited, thermally buckled plates
2. High-intensity acoustic tests of a thermally stressed plate
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