本文采用NUMECA的FINE/Turbo软件包数值分析了一个高压比离心叶轮的三维定常粘性流场.选用二阶精度的中心格式和Spalart-Allmaras的一方程湍流模型.通过与现有实验结果(包括性能曲线、外环壁静压和截面马赫数分布等)的比较对计算结果就行了详细的确认,同时讨论了网格密度和间隙尺度、以及不同的数据处理方法对计算结果确认的影响.
参考文献
[1] | Hathaway M D;Chriss R M;Strazisar A J et al.Laser Anemometer Measurements of the Three-Dimensional Rotor Flow Field in the NASA Low-Speed Centrifugal Compressor: NASA Technical Paper[R].ARL-TR-333,1995. |
[2] | Krain H .Swirling Impeller Flow[J].Journal of Turbomachinery,Transactions of the ASME,1988,110:122-128. |
[3] | KANG S;Hirsch C .Numerical Simulation and Theoretical Analysis of the 3D Viscous Flow in Centrifugal Impellers. Invited Lecture Presented in the 5th ISAIF, Gdansk,Poland, 2001[J].Journal TASK Quarterly Poland,2001,5(04):455-479. |
[4] | Krain H;Hoffman B.Aerodynamic of Centrifugal Compressor with Transonic Flow[M].VKI Lecture Series "Flow in Radial Turbomachines",1996 |
[5] | Eisenlohr G;Krain H .Investigation of the Flow Through a High Pressure Ratio Centrifugal Impeller[R].ASME 2003-GT-30394,2003. |
[6] | Senoo Y;Hayami H;Kinoshita Y et al.Experimental Study on Flow in a Supersonic Centrifugal Impeller[J].Journal of Engineering for Power-Transactions of the ASME,1979,101:32-41. |
[7] | Krain H .Private Communication[Z].,1996. |
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