Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds
Author:
Affiliation:
1. Langley Aeronautical Laboratory, NACA
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3908
Reference37 articles.
1. Hayes, W., A Buckled Plate in a Supersonic Stream, North American Aviation Report AL-1029, M a y 10, 1950.
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