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两种多重网格法求解径流叶轮机械可压流动
引用本文:衣同训,姜勇,索沂生. 两种多重网格法求解径流叶轮机械可压流动[J]. 推进技术, 2000, 21(6): 52-55
作者姓名:衣同训  姜勇  索沂生
作者单位:清华大学,热能工程系,北京,100084
基金项目:兵器工业部预研基金项目! (2 0 2 1C 910 6 )
摘    要:
为了加快数值求解叶轮机械内部流场的收敛速度,并改善计算结果,在数值求解径流叶轮机械可压流动的计算中,采用了由微元、二重和三重网格逐级转入和同时转入的两种多重网格法。对德国宇航局Krain H设计的离心压气机内部流场的数值计算表明,两种多重网格法的计算结果差别不大,尽管在收敛速度方面存在差异,但均与测量数据吻合比较好。

关 键 词:径向流 流场仿真 多重网格 时间推进 叶轮机械

Comparison of two multi-grid schemes for radial turbo-machinery compressible flow
Yi Tongxun,Jiang Yong and Suo Yisheng. Comparison of two multi-grid schemes for radial turbo-machinery compressible flow[J]. Journal of Propulsion Technology, 2000, 21(6): 52-55
Authors:Yi Tongxun  Jiang Yong  Suo Yisheng
Affiliation:Dept of Thermal Engineering,Tsinghua Univ ,Beijing 100084,China;Dept of Thermal Engineering,Tsinghua Univ ,Beijing 100084,China;Dept of Thermal Engineering,Tsinghua Univ ,Beijing 100084,China
Abstract:
To accelerate the converging process of turbomachinery CFD and improve the calculation results, two new multi-grid schemes are used to calculate the internal flow field inside the radial turbomachinery The calculation of Krain H centrifugal impeller shows that the simulation results of the two methods are very similar and both fit fairly well with the measurement In addition, both methods greatly improve the converging speed while some difference exists between the two methods in converging process
Keywords:Radial flow  Flow field simulation  Multiple grid scheme  Explicit time marching method
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