hypersonic shock tunnel 高超声速激波管
high-enthalpy shock tunnel 高焓激波管 ; 高焓激波风洞
a shock tunnel 激波风洞
shock-tunnel simulation 激波风洞模型试验
hypervelocity shock tunnel 极高速激波管
free-piston shock tunnel 自由活塞激波风洞
free piston shock tunnel 游动活塞式激波风洞
electric arc shock tunnel 电弧式激波风洞
A combination facility, which consists of a shock tunnel and a shock tube, was used for studying ignition and supersonic combustion of premixed hydrocarbon fuel-air mixture.
采用激波风洞-激波管组合设备对预混的碳氢燃料——空气混合物的点火与超声速燃烧进行了研究。
This paper presents experimental results of flap heat transfer and pressure characteristics on a blunt cone in shock tunnel.
本文介绍了一种在激波风洞中取得的，装在钝锥模型上的控制翼热流及压力特性实验结果。
In this paper, basic composition, design methods, and debugging situation of a supersonic MHD technical experimental system based on shock tunnel are introduced.
基于此，介绍了基于激波风洞的超声速磁流体动力技术实验系统的基本组成、设计思想和调试情况。
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