blade wake

基本解释

The rigid-wake mode of co-axial rotor in forward flight was set up based on analysis of infinite blade rigid-wake mode.
采用无限片桨叶的固定尾迹分析法，建立了前飞状态下共轴双旋翼的固定尾迹模型，对共轴双旋翼的前飞气动特性进行了理论研究。
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.
基于小型轴流压气机实验台，运用热线风速仪（HWA），对不同转速、流量工况下，静叶排出口尾迹流动特性进行实验研究。
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.
为了详细研究悬停旋翼桨尖涡的形成与发展过程，以及旋翼状态参数与桨尖涡及其尾迹的关系，开展了桨尖涡及其尾迹的测量和研究。