Effects of Different Axial Position of Bleeding Airon Circulation Casing Treatment
1.School of Power and Energy,Northwestern Polytechnical University,Xi’an 710072,China;2.Collaborative Innovation Center of Advanced Aero-Engine,Beijing 100191,China
[1] Smith L H, R G Jr Griffin. Experimental Evaluation of Outer Case Blowing or Bleeding of a Single Stage Axial Flow Compressor,Part I:Design of Rotor Blowing and Bleeding Configurations[R]. NASA-CR-54587, 1966.
[2] Smith L H, C C Jr Koch. Experimental Evaluation of Outer Case Blowing or Bleeding of a Single Stage Axial Flow Compressor, Part VI: Final Report[R]. NASA-CR-54592, 1970.
[3] Freeman C, Wilson A G, Day I J, et al. Experiments in Active Control of Stall on an Aeroengine Gas Turbine[J]. Journal of Turbomachinery, 1998, 120(4): 637-647.
[4] Hathaway Michael D. Self-Recirculating Casing Treatment Concept for Enhanced Compressor Performance[R]. ASME GT-2002-30368.
[5] Yang H, Nuernberger D, Nicke E, et al. Numerical Investigation of Casing Treatment Mechanisms with a Conservative Mixed-Cell Approach[R]. ASME GT-2003-38483.
[6] Strazisar A J, Bright M M, Thorp S, et al. Compressor Stall Control Through Endwall Recirculation[R]. ASME GT-2004-54295.
[7] Weichert S, Day I, Freeman C. Self-Regulating Casing Treatment for Axial Compressor Stability Enhancement[R]. ASME GT-2011-46042.
[8] 张皓光, 楚武利, 吴艳辉, 等. 压气机端壁自适应流通延迟失速的数值分析[J]. 推进技术, 2009, 30(2):202-208.
[9] 张皓光, 楚武利, 吴艳辉, 等. 自适应流通机匣处理改善压气机性能的机理[J]. 推进技术, 2010, 31(3): 301-308.
[10] Wang W, Chu W L, Zhang H G, et al. Experimental Study of Self-Recirculating Casing Treatment in a Subsonic Axial Compressor[J]. Journal of Power and Energy, 2016, 230(8): 805-818.
[11] 李继超, 刘 乐, 张宏伟, 等. 低速单级轴流压气机自引气扩稳实验[J]. 航空动力学报, 2012, 27(11):2577-2584.
[12] Yang Chengwu, Zhao Shengfeng, Lu Xingen, et al. Investigation on Multiple Cylindrical Holes Casing Treatment for Transonic Axial Compressor Stability Enhancement[J]. Journal of Thermal Science, 2014, 23(4):346-353.
[13] 张皓光, 安 康, 谭 峰, 等. 自循环机匣处理轴向引气位置影响扩稳能力的机理[J]. 航空动力学报, 2017, 32(4): 983-989.
[14] 吴艳辉, 杨国伟, 王 博, 等. 轴向引气位置对自循环机匣扩稳的能力的影响机制研究[C]. 大连:中国航天空天动力联合会议, 2017.
[15] Reid M R D. Design and Overall Performance of Four Highly-Loaded, High-Speed Inlet Stages for an Advanced, High-Pressure-Ratio Core Compressor[R]. NASA-TP-1337, 1978.
[16] Celestina M L, Suder K L. Experiment and Computational Investigation of the Tip Cleaeance Flow in a Transonic Axial Compressor Rotor[R]. ASME Journal of Turbomachinery, 1997, 118: 218-229.
[17] 张燕峰. 高载荷压气机端壁流动及其控制策略研究[D]. 西安:西北工业大学, 2010.
[18] Denton J D. Lessons from Rotor 37[J]. Journal of Thermal Science, 1996, 6(1).
[19] Suder K L, Celestina M L. Experiment Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss[R]. NASA-TM-107310, 1996.
[20] 王 维. 轴流压气机叶顶喷气和自循环机匣处理的设计规律及流动机理研究[D]. 西安:西北工业大学, 2016.