首页> 外文会议>ASME Fluids Engineering Division summer conference;FEDSM2009 >Secondary flows in centrifugal pump impellers: PIV measurements and CFD computations
【24h】

Secondary flows in centrifugal pump impellers: PIV measurements and CFD computations

机译:离心泵叶轮中的二次流:PIV测量和CFD计算

获取原文

摘要

Two-dimensional Particle Image Velocimetry measurements and three-dimensional Computational Fluid Dynamics (CFD) analyses have been performed of the flow field inside the impeller of a low specific-speed centrifugal pump operating with a vaneless diffuser. Flow rates ranging from 80% to 120% of the design flow rate are considered in detail.It is observed from the velocity measurements that secondary flows occur. These flows result in the formation of regions of low velocity near the intersection of blade suction side and shroud. The extent of this jet-wake structure decreases with increasing flow rate.Velocity profiles have also been computed from Reynolds-averaged Navier-Stokes equations with the Spalart-Allmaras turbulence model, using a commercial CFD-code. For the considered flow rates the qualitative agreement between measured and computed velocity profiles is very good. Overall, the average relative difference between these velocity profiles is around 7%.Additional CFD computations have been performed to assess the influence of Reynolds number and shape of the inlet velocity profile on the computed velocity profiles. It is found that the influence of Reynolds number is mild. The shape of the inlet profile only has a weak effect at the shroud.
机译:已经对使用无叶扩散器的低比转速离心泵叶轮内部的流场进行了二维粒子图像测速测量和三维计算流体动力学(CFD)分析。详细考虑了设计流量的80%至120%的流量。 从速度测量中观察到发生二次流动。这些流动导致在叶片吸力侧与护罩的相交附近形成低速区域。这种喷射-尾流结构的程度随着流速的增加而减小。 还使用商业CFD代码通过Spalart-Allmaras湍流模型根据雷诺平均Navier-Stokes方程计算了速度分布。对于考虑的流速,测量和计算的速度曲线之间的定性一致性非常好。总体而言,这些速度曲线之间的平均相对差约为7%。 已经执行了额外的CFD计算,以评估雷诺数和入口速度曲线的形状对计算出的速度曲线的影响。发现雷诺数的影响是轻微的。进气口轮廓的形状仅对导流罩产生微弱的影响。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号