Nonstationary supersonic flow around a body

被引:0
|
作者
Svettsov, VV [1 ]
机构
[1] Russian Acad Sci, Inst Dynam Geospheres, Moscow 117334, Russia
关键词
Vortex; Mach Number; Stationary Flow; Supersonic Flow; Flow Parameter;
D O I
10.1134/1.1259554
中图分类号
O59 [应用物理学];
学科分类号
摘要
It is found that a nonstationary regime of supersonic flow around bodies that differs radically from the standard stationary flow can occur for high Mach numbers and low specific heat ratios of a gas. This regime is characterized by large-scale vortices in a shock-compressed region in front of the body, a curved shock-wave profile, and oscillation of all flow parameters. (C) 1999 American Institute of Physics. [S1063-7842(99)01912-1].
引用
收藏
页码:1484 / 1486
页数:3
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