an investigation made on the rotor blade tip vortex through use of a three dimensional laser doppler velocimetry(3d ldv) is described.
利用三维多谱勒激光测速仪,对悬停状态下模型旋翼桨叶附近的流场进行了实验测量。
tip vortex goes downstream outward along the span direction, and the induced drag of the wing decreases.
翼尖涡沿着展向方向向外移动,机翼诱导阻力减小。
a model is developed for the calculation of the initial rotor tip vortex core radius aiming at eliminating the empirical parameters of the tip vortex in rotor free-vortex wake analysis.
in lifting-surface theory, the non-liner phenomena of the trailing vortex in the transition wake area and of the tip vortex separation are considered.
在计算中,对于升力面理论,本论文考虑了过渡区尾涡收缩和叶梢分离的非线型现象的影响;
this paper studied the velocity field of a forward swept axial-flow fan with no casing configuration by means of piv technology, and a tip vortex phenomenon is observed.
本文利用对开式前缘弯掠轴流风扇进行piv实验,捕捉到了开式轴流风扇的叶尖涡。
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.