炮风洞 meaning in Chinese

gun tunnel

A hypersonic pulse tunnel is designed in this paper , which has multiple running modes based on gun tunnel and shock tube theory
本文设计了一座具有多种运行方式的高超声速大型脉冲风洞,该风洞可以采用炮风洞和激波管两种运行方式。
The code calibration is completed by comparing the numerical results with data from two experiments , one of which is test of a 2 - d hypersonic inlet with internal compression and the other a sidewall compression inlet . good agreement of numerical and experimental results proves the possibility and credibility of the numerical method
利用国外文献公布的二维进气道实验结果和本课题组侧压式进气道炮风洞实验获得的实验数据对本文的计算方法进行了校验,证明了本文所采用的方法应用于高超声速进气道计算的可行性和可靠性。