研究结果表明：旋翼的拉力大约增加4%，旋翼的下洗载荷相当于整个旋翼拉力的10%左右。
The results of research show that the rotor thrust increase 4% and the download force on the wing can be as large as 10 percent of the total rotor thrust.
利用旋臂式模型机动飞行试验机进行倾转过渡状态下旋翼瞬态拉力的试验研究，试验与理论计算结果表现出很好的相关性。
The experiment of transient rotor thrust during transition flight has been carried out on whirling beam test facility, and the experimental results show excellent agreement with theory.
旋翼机与直升机不同，它的旋翼和发动机没有联系，不能提供拉力和操纵力矩。
Gyroplane is different from the helicopter. Its rotors are not linked to the engine and cannot provide pulling force and controlling moment.
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