机翼表面压力 meaning in Chinese

pressure on wing

In order to understand the rotor / wing interaction each other , firstly , the change of the isolate rotor thrust with the collective pitch and rotate speed is tested , secondly , the change of the rotor thrust with the collective pitch , rotate speed and the wing / rotor distance is scaled , when the wing is placed underside the rotor , lastly , the pressure on the wing due to the rotor wake is scaled
为了搞清楚它们之间的相互影响，本文首先测量孤立旋翼的拉力随总距和转速的变化；再测量有机翼时旋翼的拉力随总距及转速的变化以及随旋翼机翼间的距离变化；最后测量旋翼尾流对机翼表面压力的影响。
This paper explored the micro pressure sensor that is used for the measurement of distributed pressure at the surface of smart - skin . firstly , established the surface pressure model according to the aerodynamic properties , defined the optical measurement system that based on intensity modulation principle , discussed the components of this system and theoretical analyzed its measurement theory in detail
首先，根据空气流动的基本规律给出机翼表面压力分布图，通过对光学式微型压力传感器的理论分析，采用强度调制法测量飞机机翼表面的压力并建立基于此方法的光学测量系统模型，得到了压力与敏感膜片变形以及光电转换输出能量之间的关系。