Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression

被引：0
|
作者：
V. M. Galkin
D. A. Vnuchkov
V. I. Zvegintsev
机构：
[1] Tomsk Polytechnical University,Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
[2] Russian Academy of Sciences,undefined
来源：
Journal of Applied Mechanics and Technical Physics | 2015年 / 56卷
关键词：
supersonic flow; axisymmetric tunnel air inlet; Euler equations; method of characteristics; isentropic expansion; viscous flow;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A method of designing a supersonic axisymmetric tunnel air inlet based on the problem of an inverted flow in an annular nozzle with isentropic expansion is considered. The nozzle contour is constructed by the method of characteristics. Parameters of one inlet for viscous and inviscid gas flows are calculated.
引用
收藏
页码：831 / 837
页数：6
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