Results show that the method is useful for the aerodynamics design of jet vane and ignition experiments of the aided engine 该文所用方法对于燃气舵的气动设计、辅助发动机点火试验具有指导意义。
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A 3 - d viscosity turbulence model is used to analyze the unsteady around flow field of the thrust - vectoring engine of the jet vane , and results of the area including vane base , vane flake and motor shell are presented 摘要以推力矢量发动机的燃气舵为研究对象，采用三维、粘性、湍流流动模型和数值分析的接触网格技术，在定常流动计算的基础上，对包含舵基、舵片和发动机壳体的区域进行详细数值分析。
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