The principle of the method and its calculation processes are discussed, and results of a stable jet flame temperature distribution are given.
文中讨论了这一方法的基本原理及实现过程，并给出了对稳态射流火焰的实测结果。
So the problem of taking the picture of real rocket jet with high temperature, high velocity and strong flame was solved.
解决了长期以来无法拍摄到高温、高速、强火焰光的火箭射流流场图像的问题。
In order to achieve a rapid initiation of detonation in a short distance, a flame jet ignition system was applied to the pulse detonation rocket engine (PDRE).
为了实现快速短距起爆，火焰射流点火系统被尝试应用在脉冲爆震火箭发动机上。
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