scramjet inlet

基本解釋

An experimental study was carried out on three-dimensional scramjet inlet flow.
本文主要進行超燃沖壓發(fā)動機三面壓縮進氣道的實驗研究。
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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)動機二維進氣道的多級多目標設計方法。
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.
在此基礎上建立了一體化超燃沖壓發(fā)動機進氣道、隔離段、燃燒室及尾噴管計算模型，并對一體化設計的超燃沖壓發(fā)動機模型進行了初步計算。