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周军伟 杨荣菲 侯安平 周盛. 压气机近失速点旋涡流场时空演化分析[J]. 力学学报, 2010, 42(4): 623-628. DOI: 10.6052/0459-1879-2010-4-lxxb2009-056
引用本文: 周军伟 杨荣菲 侯安平 周盛. 压气机近失速点旋涡流场时空演化分析[J]. 力学学报, 2010, 42(4): 623-628. DOI: 10.6052/0459-1879-2010-4-lxxb2009-056
Time-space analysis of vortex flow field in compressor at near-stall point[J]. Chinese Journal of Theoretical and Applied Mechanics, 2010, 42(4): 623-628. DOI: 10.6052/0459-1879-2010-4-lxxb2009-056
Citation: Time-space analysis of vortex flow field in compressor at near-stall point[J]. Chinese Journal of Theoretical and Applied Mechanics, 2010, 42(4): 623-628. DOI: 10.6052/0459-1879-2010-4-lxxb2009-056

压气机近失速点旋涡流场时空演化分析

Time-space analysis of vortex flow field in compressor at near-stall point

  • 摘要: 为了探索轴流压气机内旋涡流场的时空演化特征, 对一台压气机转子的流场进行了时间精确的数值模拟. 通过对转子不同轴向位置的流量分析发现, 在压气机近失速工况附近, 压气机进口流量波动约为最大流量的2%. 对旋涡流场的进一步分析发现, 叶片尾缘附近吸力面的旋涡流场摆动是导致压气机进口流量波动的主要原因.

     

    Abstract: In order to study the time-space characteristics of vortexflow field in axial compressor, a time-critical CFD method was employed tonumerically simulate the flow field in a single rotor. After the mass flowanalysis at different axial positions in the rotor, it is found that thefluctuation value of inlet mass flow is 2% normalized by the maximum massflow. In addition, it is also found that the oscillation of vortex flowfield at suction side near the trailing edge was the main reason for theinlet mass flow fluctuation.

     

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