Three-dimensional effects and the interaction between an obstacle and a shock wave discharged from a channel

被引:2
|
作者
Bazhenova, TV [1 ]
Bormotova, TA [1 ]
Golub, VV [1 ]
Kotel'nikov, AL [1 ]
Chizhikov, AS [1 ]
Shcherbak, SB [1 ]
机构
[1] Russian Acad Sci, IVTAN Inst High Temp Sci Assoc, Inst High Energy Dens, Moscow 127412, Russia
基金
俄罗斯基础研究基金会;
关键词
Statistical Physic; Shock Wave; Mach Number; Total Pressure; Numerical Investigation;
D O I
10.1023/A:1015251122879
中图分类号
O59 [应用物理学];
学科分类号
摘要
The results are given of experimental and numerical investigations of the total pressure across a stagnation shock in the flow C, behind a shock wave discharged from open ends of round and square channels. It is found that the loss of total pressure behind a stagnation wave before an obstacle when discharged from a square channel exceeds that in the case of a round channel. The observed effect is attributed to the fact that, when a shock wave is discharged from a square channel, the flow separation occurs at a greater angle, which is accompanied by an increase in the Mach number of the flow.
引用
收藏
页码:222 / 227
页数:6
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