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)的螺旋槳?jiǎng)恿坷碚撆c計(jì)算流體力學(xué)的方法相結(jié)合，數(shù)值模擬螺旋槳滑流對(duì)其后部件氣動(dòng)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(guó)產(chǎn)雙渦槳支線(xiàn)飛機(jī)發(fā)展過(guò)程中，曾專(zhuān)門(mén)研究過(guò)螺旋槳滑流對(duì)飛機(jī)表面壓力分布的影響。
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.
引入基于動(dòng)量理論的激勵(lì)盤(pán)模型，通過(guò)求解三維雷諾平均的N-S方程，數(shù)值模擬了螺旋槳滑流對(duì)帶發(fā)動(dòng)機(jī)短艙的機(jī)翼氣動(dòng)特性的影響，并與實(shí)驗(yàn)值進(jìn)行了對(duì)比分析。