Application of Improved k-ω-γ Transition Model to Hypersonic Complex Configurations

被引:19
作者
Zhou, Ling [1 ]
Zhao, Rui [1 ]
Yuan, Wu [2 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] Chinese Acad Sci, Sch Aerosp Engn, Beijing 100190, Peoples R China
基金
中国国家自然科学基金;
关键词
MODULAR RANS APPROACH; BOUNDARY-LAYER; LOCAL VARIABLES; FLOW TRANSITION;
D O I
10.2514/1.J057609
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:2214 / 2221
页数:8
相关论文
共 20 条
[1]  
Anderson J.D., 1989, HYPERSONIC HIGH TEMP, P271
[2]  
Berry S. A., 1999, 33 THERM C, DOI [10.2514/6.1999-3560, DOI 10.2514/6.1999-3560]
[3]  
Berry S. A., 2008, 38 FLUID DYN C EXH, DOI [10.2514/6.2008-3736, DOI 10.2514/6.2008-3736]
[4]  
Borg M., 2009, AIAA PAPER 2009 0396, DOI [10.2514/6.2009-396, DOI 10.2514/6.2009-396]
[5]   Effect of Freestream Noise on Roughness-Induced Transition for the X-51A Forebody [J].
Borg, Matthew P. ;
Schneider, Steven P. .
JOURNAL OF SPACECRAFT AND ROCKETS, 2008, 45 (06) :1106-1116
[6]  
Hank J., 2008, 15 AIAA INT SPACE PL, P2540, DOI [10.2514/6.2008-2540, DOI 10.2514/6.2008-2540, /10.2514/6.2008-2540]
[7]   A correlation-based transition model using local variables -: Part II:: Test cases and industrial applications [J].
Langtry, R. B. ;
Menter, F. R. ;
Likki, S. R. ;
Suzen, Y. B. ;
Huang, P. G. ;
Volker, S. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2006, 128 (03) :423-434
[8]   Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes [J].
Langtry, Robin B. ;
Menter, Florian R. .
AIAA JOURNAL, 2009, 47 (12) :2894-2906
[9]   Modelling flow transition in a hypersonic boundary layer with Reynolds-averaged Navier-Stokes approach [J].
Liang, Wang ;
Song, Fu .
SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY, 2009, 52 (05) :768-774
[10]   Transition modelling for general purpose CFD codes [J].
Menter, F. R. ;
Langtry, R. ;
Voelker, S. .
FLOW TURBULENCE AND COMBUSTION, 2006, 77 (1-4) :277-303