hypersonic inlet meaning in English

高超音速进气道
高超音速进气口

Back pressure propagation mode and maximum working back pressure of hypersonic inlet isolator
高超声速进气道隔离段反压的前传模式及最大工作反压
Cross - section design of a controllable hypersonic inlet . the research is being done at the nanjing university of aeronautics and astronautics
南京航空航天大学正在进行一个可控高超音速进气道断面设计研究。
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。