本文采用理论分析、数值模拟与实验相结合的方法对合成射流流动机理及推力向量控制中的应用进行研究。
In this paper, the flow mechanism and the applications of thrust vectoring using synthetic jet are studied in theory, numerical simulation and experiment.
不过，后休克的流动，在射流仍会亚音速。
However, after the shock the flow in the jet will still be subsonic.
根据射流动力学理论，分析了产生这种波系结构和流场压力变化的原因。
The reasons of forming a shock-cell structure and changing the flow field pressure were analyzed with jet dynamics.
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