Drag and Thrust 拖曳力与推进力
In aerodynamic terms, lift is a function of weight, thrust and drag (air resistance).
在空气动力学上,升力是重量,推力和阻力(空气阻力)的相关的函数。
If thrust and drag do not equal each other, the airplane can not fly at a constant speed.
如果推力和阻力彼此不相等,飞机就不同能等速飞行。
The configuration also provides acoustic shielding and, at low speed, increases aircraft lift without a thrust or drag penalty.
该构造还提供声屏蔽,并且在低速下,增加飞机升力的同时没有推力或阻力损失。
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