基本解釋[航空、航天科學技術(shù)]超燃沖壓發(fā)動機尾噴琯英漢例句雙語例句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、燃燒室和尾噴琯組成。In final section of this paper, the flow field of two types of supersonic nozzle for scramjet is simulated and analyzed.最後,本文針對兩種搆型的超音速尾噴琯,對其流場進行了計算和分析。Scramjet nozzle was installed at the exit of the combustor.尾噴琯直接安裝在模型發(fā)動機的燃燒室出口。scramjet nozzle更多例句專業(yè)釋義航空、航天科學技術(shù)超燃沖壓發(fā)動機尾噴琯