The aerodynamics design process of jet vane of the thrust-vector motor is discussed by combining the practical engineering.
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 obtained solution of the extracted hydrocarbons into the solvent represents a synthetic fuel, which could be used after slight reforming as motor fuel, jet fuel, or the like.
所获得的被萃取到所述溶剂中的烃的溶液表现为合成燃料，其可以在轻度转化之后用作汽车燃料、喷气燃料等。
According to the different motor ignition states, a series of total pressure values of observed points on the respective jet axis distances was measured.
针对不同的发动机点火状态，在射流轴线的不同距离上对一系列测点位置的总压参数进行了测量。
Therefore, this research would provide a instructive reference straight for the structure design of thrust-vectoring motor and jet et vane.
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。
Using the numerical analyzing method, this article studied on the problem of the thrust-vectoring motor jet flow field.
文中针对推力矢量发动机燃气流场的流动问题，运用数值分析的方法进行了研究。
There's no reason why the compressor and turbine blades in a jet engine can't be driven by an electric motor to generate thrust under water, he says.
在为引擎装备了转子叶片和调速齿轮后，涡轮轴发动机单元可以在空中和水下为飞行器提供“可接受的工作效率”，他们称。
There's no reason why the compressor and turbine blades in a jet engine can't be driven by an electric motor to generate thrust under water, he says.
在为引擎装备了转子叶片和调速齿轮后，涡轮轴发动机单元可以在空中和水下为飞行器提供“可接受的工作效率”，他们称。
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