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- W2365882016 abstract "Three popular turbulence models are compared by simulating the complex supersonic flows around long ogive-cylinder missile.A newly developed flux splitting scheme-AUSM~+-up,is adopted to obtain high resolution and robustness.The numerical results show the capability of individual turbulence model in dealing with cross separation and vortices.S-A model under-predict the cross separation and can not capture the subtle secondary vortices correctly.SST model is compared to EASM model in capturing cross separation,however not as clearly as EASM in simulating the secondary vortices. But the integrated aerodynamic forces are similar for three models,and are within ±3% agreement with experimental data.Higher Mach number can lead to earlier boundary-layer separation along axial location,and larger vortices developing in space." @default.
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- W2365882016 date "2006-01-01" @default.
- W2365882016 modified "2023-09-23" @default.
- W2365882016 title "Comparison of three turbulence models in supersonic high-attack-angle separated flows" @default.
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