Analysis of Supersonic-Hypersonic Flutter of Lifting Surfaces at Angle of Attack
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59019
Reference38 articles.
1. Young, L. S. "Effects of Angle of Attack and Thickness Ratio on the Flutter of a Rigid Unswept Diamond-Airfoil-Section Wing at a Mach Number of 10.0," TN D-1380, Aug.1962, NASA.
2. On supersonic flow past an oscillating wedge
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