Five popular turbulence models have been tested and validated against experimental data of two turbulent flows.The models are:(1)the zero equation model of Baldwin Lomax;(2)the two equation k ε model of Jones and Launder;(3)the two equation k ω model of Wilcox;(4)the two equation k ω/k ε SST model of Menter;(5)the two scale k ε model.The benchmark flows are two transonic flows over bump geometries with shock wave/boundary layer interaction including separation.The computational results demonstrate that the SST model yields superior performance and the zero equation turbulence model does not provide satisfactory results.
Large eddy simulation of supersonic jet mixing flow
Comparison and analysis of WENO schemes base on supersonic boundary layer transition
Numerical investigation of impressible turbulent flows past airfoils
Dispersion model for incompressible turbulent flows
Numerical simulation of the breakdown process in laminar-turbulent transition of incompressible boundary layer on a flat plate
Related Author
潘宏禄
程晓丽
朱志斌
WANG Hong-bo
SUN Ming-bo
WANG Zhen-guo
LIU Chao-yang
TANG Yang-yang
Related Institution
中国航天科技集团有限公司 中国航天空气动力技术研究院
College of Aerospace Science and Engineering, National University of Defense Technology
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Science and Technology Division, Civil Aviation University of China