Numerical simulation and physical aspects of supersonic vortex breakdown

被引：0
|
作者：
Liu, C.H. [1 ]
Kandil, O.A. [1 ]
Kandil, H.A. [1 ]
机构：
[1] NASA Langley Research Cent, Hampton, United States
来源：
Computers and Fluids | 1993年 / 22卷 / 4-5期
关键词：
Compressible flow - Numerical methods - Simulation - Vortex flow;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Existing numerical simulations and physical aspects of subsonic and supersonic vortex-break-down modes are reviewed. The solution to the problem of supersonic vortex breakdown is emphasized in this paper and carried out with the full Navier-Stokes equations for compressible flows. Numerical simulations of vortex-breakdown modes are presented in bounded and unbounded domains. The effects of different types of downstream-exit boundary conditions are studied and discussed.
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页码：607 / 622
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