| [1] Shabbir A, Adamczyk J J. Flow mechanism for stall margin improvement due to circumferential casing grooves on axial compressors[J]. Journal of Turbomachinery, 2005, 127(4): 708-717.[2] Korting P, Beacher B F. Improved compressor performance using recessed clearance (trenches)[J]. Journal of Propulsion and Power, 1989, 5(4): 469-475.[3] Wilke I, Kau H P. A numerical investigation of the flow mechanisms in a high pressure compressor front stage with axial slots[J]. Journal of Turbomachinery, 2004, 126(3): 339-349.[4] Zhu J, Chu W L. The effects of bend skewed groove casing treatment on performance and flow field near endwall of an axial compressor, AIAA-2005-0809[R].Reston: AIAA, 2005.[5] Lu X G, Chu W L, Zhu J Q, et al. Analysis of the coupled flow through axial skewed slots casing treatment and rotor passage[J]. Journal of Engineering Thermophysics, 2006, 27(2): 226-228. (in Chinese)卢新根, 楚武利, 朱俊强, 等. 轴向斜缝机匣处理与转子通道之间耦合流动分析[J]. 工程热物理学报, 2006, 27(2): 226-228.[6] Azimian A R, Elder R L, McKenzie A B. Application of recess vaned casing treatment to axial flow fans[J]. Journal of Turbomachinery, 1990, 112(1): 145-150.[7] Greitzer E M, Nikkanen J P, Joslyn H D, et al. A fundamental criterion for the application of rotor casing treatment[J]. Journal of Fluids Engineering, 1979, 101(2): 237-243.[8] Wang T, Xu W, Gu C G, et al. A new type of self-adaptive casing treatment for a centrifugal compressor[C]//ASME Turbo Expo 2010: Power for Land, Sea, and Air. New York: ASME, 2010: 2065-2074.[9] Hu L J, Yang C, Sun H M, et al. Effect of casing treatment on the centrifugal compressor shock wave/tip leakage interaction[J]. Transactions of Beijing Institute of Technology, 2010, 30(5): 521-526. (in Chinese)胡良军, 杨策, 孙惠民, 等. 机匣处理对离心压气机激波与泄漏涡干涉的影响[J]. 北京理工大学学报, 2010, 30(5): 521-526.[10] Huang G P, Liang D W, Chen J. Pre-cyclone vane type engine case processing method: China. ZL200710024378.5 [P]. 2011-04-20. (in Chinese)黄国平, 梁德旺, 陈杰. 预旋叶片式机匣处理方法: 中国. ZL200710024378.5[P]. 2011-04-20.[11] Gao P, Chu W L, Wu Y H. Stall control of a centrifugal compressor with recess vaned casing treatment[J]. Journal of Engineering for Thermal Energy and Power, 2008, 23(3): 229-234. (in Chinese)高鹏, 楚武利, 吴艳辉. 离心压气机凹槽导流片式机匣处理失速控制研究[J]. 热能动力工程, 2008, 23(3): 229-234.[12] Xiao J, Xu W, Gu C G, et al. Self-recirculating casing treatment for a radial compressor[J]. Chinese Journal of Mechanical Engineering, 2009, 22(4): 567-573.[13] Tamaki H. Effect of recirculation device with counter swirl vane on performance of high pressure ratio centrifugal compressor[J]. Journal of Turbomachinery, 2012, 134(5): 051036.[14] Shi J C, Zou X Q, Wen Q, et al. Study on new type casing treatment method for centrifugal compressor[J]. Aeroengine, 2010, 36(3): 1-4. (in Chinese)石建成, 邹学奇, 温泉, 等. 离心压气机流动控制机匣新型处理方式研究[J]. 航空发动机, 2010, 36(3): 1-4.[15] Teng J F, Zhu M M, Qiang X X. Effect of double inclined slotted casing treatment on centrifugal compressor performance[J]. Journal of Aerospace Power, 2013, 28(1): 164-170. (in Chinese)滕金芳, 朱铭敏, 羌晓青. 双倾斜壁缝式机匣处理对离心压气机性能的影响[J]. 航空动力学报, 2013, 28(1): 164-170.[16] Kang J X. Improved design and experimental in-vestigation for the centrifugal impeller of a 75 kW gas turbine engine[D]. Shanghai: Shanghai Jiaotong University, 2008. (in Chinese)康剑雄. 75 kW燃气轮机离心叶轮改进设计及试验研究[D]. 上海: 上海交通大学, 2008.[17] Ning F F, Fan L. Quasi-steady flow model of slot-type casing treatmentsⅠ: modeling method and validation[J]. Journal of Aerospace Power, 2012, 27(6): 1261-1269. (in Chinese)宁方飞, 樊琳. 一种槽道式处理机匣的准定常流动模型Ⅰ: 建模方法及验证[J]. 航空动力学报, 2012, 27(6): 1261-1269.[18] Vo H D, Tan C S, Greitzer E M. Criteria for spike initiated rotating stall[J]. Journal of Turbomachinery, 2008, 130(1): 011023. |
CJA
