Interaction of shock wave with subsonic heated layer

被引：0
作者：
V. N. Zudov
机构：
[1] Russian Academy of Sciences,Institute of Theoretical and Applied Mechanics, Siberian Branch
来源：
Technical Physics Letters | 2010年 / 36卷
关键词：
Shock Wave; Mach Number; Technical Physic Letter; Supersonic Flow; Incident Shock Wave;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The problem of attenuation of an incident shock wave on the passage through a heated layer of finite thickness has been considered by numerical methods. Three possible regimes of interaction of the incident shock wave with the heated layer are revealed. It is shown that a significant decrease in intensity of the incident shock wave is caused by its interaction with a heated subsonic jet trace.
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页码：868 / 871
页数：3
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