Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum Angle of attack, the flap Angle and the wind over the deck on...
最后讨论了飞机的起飞质量，发动机推力、起飞迎角、襟翼偏角和甲板风航迹等对弹射起飞性能的影响。
The optimization of maximum attack Angle is evaluated according to the given initial design parameters by using the orthogonal method.
最大攻角的优化根据给定的初始设计值采用正交法进行。
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