Viscous supersonic flow around an exterior obtuse angle

被引：0

作者：

Chefanov, VM ^{[1
]}

机构：

[1] Kazan State Tech Univ, Kazan, Russia

来源：

IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA | 2001年 / 02期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

We present the results of the theoretical analysis of the boundary layer behavior in the supersonic flow around the contour discontinuity. The results can be applied in the design of supersonic nozzles with the contour discontinuity in the nozzle throat.

引用

页码：21 / 24

页数：4

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