scramjet inlet

基本解释

An experimental study was carried out on three-dimensional scramjet inlet flow.
本文主要进行超燃冲压发动机三面压缩进气道的实验研究。
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A multi-level and multiobjective optimization (MLMOO) design method for two-dimensional scramjet inlet was established.
提出了超燃冲压发动机二维进气道的多级多目标设计方法。
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.
在此基础上建立了一体化超燃冲压发动机进气道、隔离段、燃烧室及尾喷管计算模型，并对一体化设计的超燃冲压发动机模型进行了初步计算。