Model Reduction of Computational Aerothermodynamics for Hypersonic Aerothermoelasticity
Author:
Affiliation:
1. Ohio State University, Columbus, Ohio 43210
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051094
Reference27 articles.
1. Piston Theory-A New Aerodynamic Tool for the Aeroelastician
2. From Piston Theory to a Unified Hypersonic-Supersonic Lifting Surface Method
3. Unsteady Unified Hypersonic-Supersonic Aerodynamics: Analytical and Expedient Methods for Stability and Aeroelasticity
4. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future
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