摘要
应用激光多普勒测速仪和旋转编码器实现了对后弯闭式离心叶轮内三维湍流流场的测量。较详细地描述了设计工况下回转流面上主流速度的分布特点 ;绘出了径向流面上速度矢量分布图 ,结果表明在旋转流场中 ,流体粘性对气流方向具有不可忽视的作用 ;实验测量还得到了在曲率和旋转因素的综合作用下 ,流道中部和出口处产生的由强到弱的二次流涡 。
A Laser Doppler Velocimeter (LDV) and shaft encoder was used to measure velocities at the design flow of the shrouded centrifugal backswept impeller.Measurements of the three-dimensional velocity field were acquired at several main planes through the passage.The measurements described both the through flow velocity field along circumferential measurement planes and the velocity vector at radial planes.It was found that the high velocity flow was held near the hub side on the suction surface of blade passage and shifted from the hub to the shroud side on the pressure surface as the fluid approached the exit.The results also provided the evidence of the development of a 'wake' of low momentum fluid near the shroud at midpitch at the exit.The velocity vector plots showed that the flow angles on the hub were very differential from those on the shroud side because of the fluid viscosity.The results indicated that the secondary flow generated in vertical direction of the main flow velocity was related to curvature and rotating of impeller.The secondary flow velocity vector plots were also presented at the middle passage and exit.The development of the secondary vortex along impeller blade passage has been clearly observed and recorded.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2002年第3期287-291,共5页
Journal of Aerospace Power
