Optimization of Information Gain in Multifidelity High-Speed Pressure Predictions
Author:
Affiliation:
1. Vanderbilt University, Nashville, Tennessee 37235
2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J059507
Reference21 articles.
1. Studies on Fluid-Thermal-Structural Coupling for Aerothermoelasticity in Hypersonic Flow
2. Quantifying Model Discrepancy in Time-Dependent, Coupled Analyses
3. Piston Theory-A New Aerodynamic Tool for the Aeroelastician
4. Issues in Deciding Whether to Use Multifidelity Surrogates
5. Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function
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