旋转机翼飞机是一种新概念飞行器，是旋翼飞行器和固定翼飞行器的结合。
Rotor wing plane is a new concept of aircraft, and is the combination of rotor aircraft and fixed wing aircraft.
旋翼干扰空气动力学问题一直是旋翼飞行器空气动力学的研究热点和难点之一。
Research on the aerodynamic interaction between the rotors and components of rotorcraft have been a very important aspect and a very challenging subject in rotorcraft Aerodynamics.
结果表明：本文所述方法能合理地给出倾转旋翼飞行器在整个稳定飞行速度范围内的操纵量和姿态。
The number of total layer, impulse of each impulse engine and fire interval are determined when the correct ability and flight stability are satisfiable.
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