scramjet nozzle

基本解釋

• [航空、航天科學(xué)技術(shù)]超燃沖壓發(fā)動機(jī)尾噴管

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(jī)由進(jìn)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(jìn)行了計(jì)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(jī)的燃燒室出口。

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專業(yè)釋義

航空、航天科學(xué)技術(shù)

• 超燃沖壓發(fā)動機(jī)尾噴管