Assessment of High-Temperature Effects on Hypersonic Aerothermoelastic Analysis using Multi-Fidelity Multi-Variate Surrogates
Author:
Affiliation:
1. Pennsylvania State University
2. University of Arizona, Tucson
Publisher
American Institute of Aeronautics and Astronautics
Reference53 articles.
1. George Tzong, Richard Jacobs, and Salvatore Liguore, “Predictive Capability for Hypersonic Structural Response and Life Prediction, Phase 1 - Identification of Knowledge Gaps, VolumeI,” Tech. Rep. AFRL-RB-WP-TR-2010-3068,V1, Wright-Patterson Air Force Base, Dayton, OH, Sep. 2010.
2. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future
3. Zuchowski, B. “Predictive Capability for Hypersonic Structural Response and Life Prediction: Phase II - Detailed Design of Hypersonic Cruise Vehicle Hot-Structure,” Tech. Rep. AFRL-RQ-WP-TR-2012-0280, Wright-Patterson Air Force Base, Dayton, OH, May 2012.
4. Physics Drivers of Hypersonic Vehicle Design
5. Nonequilibrium Hypersonic Aerothermodynamics
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