研究的结论可以为推力矢量发动机及燃气舵的结构设计提供直接的参考。
Therefore, this research would provide a instructive reference straight for the structure design of thrust-vectoring motor and jet et vane.
结合工程实际，论述和分析了推力矢量发动机燃气舵气动特性的设计过程。
The aerodynamics design process of jet vane of the thrust-vector motor is discussed by combining the practical engineering.
采用六分力试验技术对某推力矢量发动机燃气舵的气动特性进行了试验研究。
Computational investigation of secondary flow thrust vector control technology used in a convergent-divergent nozzle;
采用六分力试验技术对某推力矢量发动机燃气舵的气动特性进行了试验研究。
Computational investigation of secondary flow thrust vector control technology used in a convergent-divergent nozzle;
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