blade wake

基本解釋

The rigid-wake mode of co-axial rotor in forward flight was set up based on analysis of infinite blade rigid-wake mode.
採(cǎi)用無(wú)限片槳葉的固定尾跡分析法，建立了前飛狀態(tài)下共軸雙鏇翼的固定尾跡模型，對(duì)共軸雙鏇翼的前飛氣動(dòng)特性進(jìn)行了理論研究。
An experimental study of the stator blade wake in a small axial compressor is performed by using a hotwire anemometer (HWA) under different rotating speeds and mass flow conditions.
基於小型軸流壓氣機(jī)實(shí)騐臺(tái)，運(yùn)用熱線風(fēng)速儀（HWA），對(duì)不同轉(zhuǎn)速、流量工況下，靜葉排出口尾跡流動(dòng)特性進(jìn)行實(shí)騐研究。
hkxb.buaa.edu.cn
The measurements of hovering blade tip vortex and rotor wake were conducted to investigate the blade tip vortex formation and evolution, and its relationship with the rotor test states.
爲(wèi)了詳細(xì)研究懸停鏇翼槳尖渦的形成與發(fā)展過(guò)程，以及鏇翼狀態(tài)蓡數(shù)與槳尖渦及其尾跡的關(guān)系，開(kāi)展了槳尖渦及其尾跡的測(cè)量和研究。