Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels

被引：0
|
作者：
S. M. Aulchenko
V. M. Galkin
V. I. Zvegintsev
A. N. Shiplyuk
机构：
[1] Russian Academy of Sciences,Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Division
[2] Oil,Institute of Geology
[3] and Gas at the Tomsk Polytechnical University,undefined
来源：
Journal of Applied Mechanics and Technical Physics | 2010年 / 51卷
关键词：
hypersonic nozzle; Navier-Stokes equations; Euler equations; method of characteristics; numerical optimization;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A method for design of hypersonic nozzles for wind tunnels is developed and implemented on the basis of solving direct problems with various models of the medium and numerical methods of integration of gas-flow equations. Multimodal nozzles for operation in Mach number ranges Mout=8–14 and Mout=14–20 satisfying specified requirements are designed.
引用
收藏
页码：218 / 225
页数：7
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