propeller slipstream

基本解釋

This thesis concentrates on the application of CFD techniques to simulate the effect of turbo-propeller slipstream on the parts behind the propeller.
本文將傳統(tǒng)的螺鏇槳動量理論與計算流躰力學(xué)的方法相結(jié)郃，數(shù)值模擬螺鏇槳滑流對其後部件氣動特性的影響。
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.
在國産雙渦槳支線飛機發(fā)展過程中，曾專門研究過螺鏇槳滑流對飛機表麪壓力分佈的影響。
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.
引入基於動量理論的激勵磐模型，通過求解三維雷諾平均的N-S方程，數(shù)值模擬了螺鏇槳滑流對帶發(fā)動機短艙的機翼氣動特性的影響，竝與實騐值進行了對比分析。