Thermal Reduced Order Model Adaptation to Aero-Thermo-Structural Interactions
Author:
Affiliation:
1. Arizona State University
2. Air Force Research Laboratory
3. Ohio State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0493
Reference12 articles.
1. Coupled Flow-Thermal-Structural Analysis for Response Prediction of Hypersonic Vehicle Skin Panels
2. Fluid-Thermal Response of Spherical Dome Under a Mach 6.59 Laminar Boundary Layer
3. Impact of Fluid-Thermal-Structural Coupling on Response Prediction of Hypersonic Skin Panels
4. Proper Orthogonal Decomposition for Reduced-Order Thermal Solution in Hypersonic Aerothermoelastic Simulations
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