NN-augmented k - ω shear stress transport turbulence model for high-speed flows with shock-wave/boundary layer interaction
Author:
Affiliation:
1. State Key Laboratory of Aerodynamics, Mianyang, People's Republic of China
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Link
https://www.tandfonline.com/doi/pdf/10.1080/19942060.2024.2374316
Reference54 articles.
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4. Wall pressure fluctuations in supersonic boundary layers over compression ramps with different turning angles
5. A prediction model of wall shear stress for ultra-high-pressure water-jet nozzle based on hybrid BP neural network
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