propeller slipstream

基本解释

This thesis concentrates on the application of CFD techniques to simulate the effect of turbo-propeller slipstream on the parts behind the propeller.
本文将传统的螺旋桨动量理论与计算流体力学的方法相结合，数值模拟螺旋桨滑流对其后部件气动特性的影响。
During the development of china-built double turboprop engines commuter aircraft, the influence has been studied which propeller slipstream affects the pressure distribution on aircraft.
在国产双涡桨支线飞机发展过程中，曾专门研究过螺旋桨滑流对飞机表面压力分布的影响。
The three dimensional RANS equations with adoption of an actuator disk model based on the momentum theory are used to simulate the effect of turbo-propeller slipstream on a wing-nacelle configuration.
引入基于动量理论的激励盘模型，通过求解三维雷诺平均的N-S方程，数值模拟了螺旋桨滑流对带发动机短舱的机翼气动特性的影响，并与实验值进行了对比分析。