后缘襟翼

采用动量理论结合有限体积法求解N-S方程的方法，进行了螺旋桨滑流对带后缘襟翼机翼气动特性干扰的数值模拟分析。

The N-S equations with adoption of an actuator disk model are used to simulate the effect of turbo-propeller slipstream on high-lift systems . The equations are solved by using the finite volume method .

在不改变巡航构型的设计原则下，对三段翼型的后缘襟翼进行优化设计。

Under the design principle of keeping the cruise configuration , the three elements airfoil is optimized .

螺旋桨滑流对带后缘襟翼机翼气动特性影响的数值分析初步探讨了二维翼型前、后缘襟翼的偏转位置对气动效率的影响。

The influence of airfoil 's leading and trailing flaps ' deflection location on aerodynamic efficiency is also discussed primarily .

本文对智能旋翼的研究主要是面向真实翼型的主动后缘襟翼智能旋翼驱动器模型设计和试验研究。

The work of this thesis is mainly about the design and test of an actuator for a smart rotor with the trailing edge configuration .

后缘襟翼位置指示器最后，他才小心翼翼地走到窗边站住，转过头来。

Trailing-edge flap position indicator Finally , he walked across the room with a measured tread to where the window was . He stopped there , and faced round .