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.

• 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。