期刊文献+

Topology and Vortex Structures of Turbine Cascade with Different Tip Clearances 被引量:5

在不同叶顶间隙下涡轮叶栅的拓扑与旋涡结构(英文)
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摘要 This paper uses the topology theory to analyze the surface flowspectrums of straight, positively curved and negatively curvedcascades with relative tip clearances of 0.023 and 0.036, findsapparent differences of topology and vortex structures in the bladetip and the suction side wall corner of single type of cascade withthis two clearances, and studies the mechanism of the differenceformation as well as their effects o the energy loss. This paper uses the topology theory to analyze the surface flowspectrums of straight, positively curved and negatively curvedcascades with relative tip clearances of 0.023 and 0.036, findsapparent differences of topology and vortex structures in the bladetip and the suction side wall corner of single type of cascade withthis two clearances, and studies the mechanism of the differenceformation as well as their effects o the energy loss.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第1期18-26,共9页 中国航空学报(英文版)
基金 ScientificResearchFoundationofHarbinInstituteofTechnology(HIT .2 0 0 0 .74) NationalDoctoralEducationFoundation
关键词 turbine cascade blade tip clearance flow visualization topology andvortex structures turbine cascade blade tip clearance flow visualization topology andvortex structures
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参考文献6

  • 1Oates G C.The aerothermodynamics of aircraft gas turbine engines[Z].ALAA Inc,1978.
  • 2Szanca R.Research turbine for high-temperature core engine application,Part Ⅱ:Effect of rotor tip clearance on overall performance[R].NASA TN D-7639,1974.
  • 3韩万今,钟兢军,黄洪雁,王仲奇.具有叶顶间隙的涡轮正弯叶栅流场的拓扑与旋涡结构[J].空气动力学学报,1999,17(2):141-149. 被引量:10
  • 4韩万今,黄洪雁,王仲奇.叶片弯曲对叶顶间隙流动影响的实验研究[J].航空学报,1999,20(5):399-404. 被引量:4
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二级参考文献4

  • 1王仲奇 工程热物理学会.一代新型轴流式透平机械叶片--叶片的弯扭联合气动成型理论及试验结果.气动热力学发展战略研讨会专题报告汇编[M].北京:中国工程热物理研究所,1989..
  • 2Kang Shun,博士学位论文,1993年
  • 3王仲奇,气动热力学发展战略研讨会专题报告汇编,1989年
  • 4韩万今,黄洪雁,侯建东,王仲奇.叶片正弯对间隙流动的影响[J].工程热物理学报,1997,18(4):429-434. 被引量:5

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