The results of experimental study on reactingflow behind a swirler by LDA are presented in this paper.
本文给出了用LDA测量旋流器后火焰流场的试验研究结果。
2
Numerical calculation model and method are applicable to analyzing reactingflow field of the solid rocket ramjet with central air-inlet mode.
采用的数值计算模型和方法适用于分析中心进气式固冲发动机反应流场。
3
Two-phase turbulent reactingflow model of the internal operating processes in Liquid Rocket Engine (LRE) is set up in non-orthogonal curvilinear coordinates.