scramjet inlet

常見例句

An experimental study was carried out on three-dimensional scramjet inlet flow.
本文主要進(jìn)行超燃沖壓發(fā)動(dòng)機(jī)三面壓縮進(jìn)氣道的實(shí)驗(yàn)研究。
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A multi-level and multiobjective optimization (MLMOO) design method for two-dimensional scramjet inlet was established.
提出了超燃沖壓發(fā)動(dòng)機(jī)二維進(jìn)氣道的多級(jí)多目標(biāo)設(shè)計(jì)方法。
Based on these efforts, primary calculating models for integrated scramjet engine inlet, separating section, combustion chamber and nozzle were built, and the primarily calculations were conducted.
在此基礎(chǔ)上建立了一體化超燃沖壓發(fā)動(dòng)機(jī)進(jìn)氣道、隔離段、燃燒室及尾噴管計(jì)算模型，并對(duì)一體化設(shè)計(jì)的超燃沖壓發(fā)動(dòng)機(jī)模型進(jìn)行了初步計(jì)算。