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轴向间距对某跨声速轴流压气机叶排间干扰的影响规律

史亚锋 吴虎 陈立新 王征 杨金广 李密

史亚锋, 吴虎, 陈立新, 王征, 杨金广, 李密. 轴向间距对某跨声速轴流压气机叶排间干扰的影响规律[J]. 航空动力学报, 2011, 26(5): 1085-1091.
引用本文: 史亚锋, 吴虎, 陈立新, 王征, 杨金广, 李密. 轴向间距对某跨声速轴流压气机叶排间干扰的影响规律[J]. 航空动力学报, 2011, 26(5): 1085-1091.
SHI Ya-feng, WU Hu, CHEN Li-xin, WANG Zheng, YANG Jin-guang, LI Mi. Effect of different axial spacing between blade rows on transonic axial compressor performance[J]. Journal of Aerospace Power, 2011, 26(5): 1085-1091.
Citation: SHI Ya-feng, WU Hu, CHEN Li-xin, WANG Zheng, YANG Jin-guang, LI Mi. Effect of different axial spacing between blade rows on transonic axial compressor performance[J]. Journal of Aerospace Power, 2011, 26(5): 1085-1091.

轴向间距对某跨声速轴流压气机叶排间干扰的影响规律

Effect of different axial spacing between blade rows on transonic axial compressor performance

  • 摘要: 对不同轴向间距下的某跨声速轴流压气机内流场在设计转速时进行了定常数值模拟,结果表明当转子与上游静子轴向间距减小时,压气机的效率和压比有明显降低,而转子和下游静子间距减小时,压气机的效率和压比反而有所提高.进一步的非定常数值模拟结果表明:①转子与上游静子轴向间距减小时,转子前激波与静子尾缘干扰增强,造成了效率和压比的下降;②转子与下游静子轴向间距减小时,由于转子尾迹通过静子叶排时的恢复效应,由尾迹造成的掺混损失会减小,效率和压比会有所提高.

     

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出版历程
  • 收稿日期:  2010-04-29
  • 修回日期:  2010-09-03
  • 刊出日期:  2011-05-28

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