Effect of Structural Parameters on Shock Wave Boundary Layer Induced Panel Flutter
Author:
Affiliation:
1. Ohio State University
Publisher
American Institute of Aeronautics and Astronautics
Reference40 articles.
1. Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds
2. Effects of Turbulent Boundary Layer on Panel Flutter
3. Interaction of a Mach 2.25 turbulent boundary layer with a fluttering panel using direct numerical simulation
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