Modification of spalart-allmaras model for shock-wave/turbulent boundary layer interaction flow

被引：0
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作者：
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing [1 ]
100191, China
不详 [2 ]
100191, China
机构：
来源：
Kung Cheng Je Wu Li Hsueh Pao | / 2卷 / 279-283期
关键词：
Adverse pressure gradient - Boundary layer interaction - Dimensionless parameters - Predictive accuracy - Shock-wave/boundary layer interactions - Spalart-Allmaras model - Supersonic turbulent boundary layers - Turbulent kinetic energy;
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页码：279 / 283
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