Metallic thermal protection system panel flutter study
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-501
Reference10 articles.
1. Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow
2. Nonlinear Flutter of Composite Panels Under Yawed Supersonic Flow Using Finite Elements
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