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.
采用無(wú)限片槳葉的固定尾跡分析法，建立了前飛狀態(tài)下共軸雙旋翼的固定尾跡模型，對(duì)共軸雙旋翼的前飛氣動(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.
基于小型軸流壓氣機(jī)實(shí)驗(yàn)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)驗(yàn)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.
為了詳細(xì)研究懸停旋翼槳尖渦的形成與發(fā)展過程，以及旋翼狀態(tài)參數(shù)與槳尖渦及其尾跡的關(guān)系，開展了槳尖渦及其尾跡的測(cè)量和研究。