Numerical Simulation of Supersonic Turbulent Separated Flows Based on <i>k–ω</i> Turbulence Models with Different Compressibility Corrections
The accurate prediction of supersonic turbulent separated flows involved in aerospace vehicles is a great challenge for current numerical simulations. Based on the <i>k–ω</i> equations, several different compressibility corrections are incorporated in turbulence models to improve their p...
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| Format: | Article |
| Language: | English |
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MDPI AG
2023-12-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/10/12/1014 |