Interaction of shock wave with subsonic heated layer

被引：4

作者：

Zudov, V. N. ^{[1
]}

机构：

[1] Russian Acad Sci, Inst Theoret & Appl Mech, Siberian Branch, Novosibirsk 630090, Russia

来源：

TECHNICAL PHYSICS LETTERS | 2010年 / 36卷 / 09期

关键词：

Shock Wave; Mach Number; Technical Physic Letter; Supersonic Flow; Incident Shock Wave;

D O I：

10.1134/S1063785010090270

中图分类号：

O59 [应用物理学];

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.

引用

页码：868 / 871

页数：4