Rapid Steady-State Hypersonic Aerothermodynamic Loads Prediction Using Reduced Fidelity Models
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio 43210
2. Leidos, Inc., Shalimar, Florida 32579
Funder
Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035969
Reference55 articles.
1. Fluid-Thermal-Structural Interaction Effects in Preliminary Design of High Speed Vehicles
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5. A Surrogate-Based Approach to Reduced-Order Dynamic Stall Modeling
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