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对飞机采用推力矢量技术，即应用二元喷管后飞机的气动特性及飞机性能和操纵性加以初步研究，给出了一些结论。
The use of thrust vector technology aircraft, that is, the application of binary nozzle aircraft aerodynamic characteristics and aircraft performance and maneuverability to be a preliminary study, gives some conclusions.