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。
应用推荐