Multifidelity Modeling for Efficient Aerothermal Prediction of Deployable Entry Vehicles

Authors :: Thomas K. West
Mario Santos
Serhat Hosder
Source :: Journal of Spacecraft and Rockets. 58:110-123
Publication Year :: 2021
Publisher :: American Institute of Aeronautics and Astronautics (AIAA), 2021.
Abstract: The objective of this work was to investigate a multifidelity modeling approach to accurately and efficiently predict the aerothermal response of a large-diameter deployable hypersonic entry vehicl...

Subjects :: Work (thermodynamics)
Hypersonic speed
symbols.namesake
Surrogate model
Space and Planetary Science
business.industry
Computer science
symbols
Aerospace Engineering
Aerospace engineering
business
Pressure coefficient
Gaussian process

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