[体]整流罩前缘;
Computation and analysis of aeroheating of scramjet inlet cowl lip
超燃冲压发动机唇口气动热计算研究与分析
inlet cowl lip skin seal is broken.
进气道唇边封严损坏。
The analysis shows that the increase of mass capture and pressure is mainly due to the MHD interaction near and up the cowl lip region.
分析表明磁场的大小和方向以及电磁作用的位置对进气道性能有重要影响;
This paper makes an analysis of the relations between J6@ series inlet cowl lip geometry and the flow separation of the lip on the basis of reference [ 1].
本文是在文献的试验基础上,分析了J6Ⅲ系列进气道唇口几何形状和唇口气流分离的关系。
英语网 · 初中英语作文
英语网 · 双语娱乐资讯
英语网 · 双语新闻
英语网 · 少儿英语故事