Aerothermoelastic Scaling Laws for Hypersonic Skin Panel Configurations with Arbitrary Flow Orientation
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057499
Reference40 articles.
1. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future
2. Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds
3. DEVELOPMENT OF A THREE-DIMENSIONAL VISCOUS AEROELASTIC SOLVER FOR NONLINEAR PANEL FLUTTER
4. Viscous and inviscid interactions of an oblique shock with a flexible panel
5. Study on Shock-Induced Panel Flutter in 2-D Laminar Flow
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