After analysing the characteristics of the aircraft aerodynamic, anti-spin module is designed. The final result is similar with that of a foreign same kind advanced aircraft.
在分析了飞机的气动特点之后,验证设计了相应的防尾旋模块,得出的结果与国外先进的同类飞机的结果相近。
After analysing the characteristics of the aircraft aerodynamic, anti-spin module is designed. The final result is similar with that of a foreign same kind advanced aircraft.
在分析了飞机的气动特点之后,验证设计了相应的防尾旋模块,得出的结果与国外先进的同类飞机的结果相近。
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