scramjet nozzle
基本解釋
- [航空、航天科學技術(shù)]超燃沖壓發(fā)動機尾噴管
英漢例句
- The scramjet is composed of inlet, isolator, combustor and nozzle.
超燃沖壓發(fā)動機由進氣道、隔離段、燃燒室和尾噴管組成。 - In final section of this paper, the flow field of two types of supersonic nozzle for scramjet is simulated and analyzed.
最后,本文針對兩種構(gòu)型的超音速尾噴管,對其流場進行了計算和分析。 - Scramjet nozzle was installed at the exit of the combustor.
尾噴管直接安裝在模型發(fā)動機的燃燒室出口。
雙語例句
專業(yè)釋義
- 超燃沖壓發(fā)動機尾噴管