EQUALIZATION OF THE DISTRIBUTION OF MACH NUMBERS IN FLOWS OF COMPRESSIBLE GAS THROUGH SUBSONIC AND SUPERSONIC NOZZLES.

被引：0
|
作者：
Lyzhin, O.V. [1 ]
机构：
[1] Zhukovskiy Inst of Aerohydrodynamics, USSR, Zhukovskiy Inst of Aerohydrodynamics, USSR
来源：
Fluid mechanics. Soviet research | 1986年 / 15卷 / 04期
关键词：
GASES - Compressibility - MATHEMATICAL TECHNIQUES - Numerical Analysis;
D O I：
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中图分类号：
学科分类号：
摘要：
A relationship between the decrease of the nonuniformity in the field of Mach numbers in the flow of compressible gas through convergent subsonic nozzle is derived as a function of the nozzle compression ratio and the exit value of M. It is shown that the decay of nonuniformities in a supersonic nozzle is much less pronounced than in a subsonic nozzle.
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页码：26 / 31
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