| Citation: | Application of adaptive treatment casing in multi-stage axial compressor[J]. Journal of Aerospace Power, 2019, 34(6): 1373-1379. doi: 10.13224/j.cnki.jasp.2019.06.020
|
| [1] |
MOORE F K,GREITZER E M.A theory of post-stall transients in axial compressors:Part Ⅰ development of the equations［J］.Journal of Engineering for Gas Turbines and Power,1986,108(1):68-76.
|
| [2] |
GREITZER E M,MOORE F K.A theory of post-stall transients in axial compressors:Part Ⅱ application［J］.Journal of Engineering for Gas Turbines and Power,1986,108(2):231-239.
|
| [3] |
VO H D.Role of tip clearance flow on axial compressor stability［D］.Cambridge,Massachusetts:Massachusetts Institute of Technology,2001.
|
| [4] |
吴艳辉,朱俊强,刘志伟.多级轴流压气机处理机匣级的探讨［J］.航空动力学报,2002,17(5):542-548.WU Yanhui,ZHU Junqiang,LIU Zhiwei.Research on the axial position of treated casing in multistage axial-flow compressors［J］.Journal of Aerospace Power,2002,17(5):542-548.(in Chinese)
|
| [5] |
TONG Z T,LIN F.The self-induced unsteadiness of tip leakage vortex and its effect on compressor stall inception［R］.ASME Paper GT2007-27010,2007.
|
| [6] |
DANNER F C T,KAU H P,MULLER M M.Experimental and numerical analysis of axial skewed slot casing treatments for a transonic compressor stage［R］.ASME Paper GT2009-59647,2009.
|
| [7] |
HAH C.Role of tip clearance flows on flow instability in axial flow compressors［R］.International Society for Air Breathing Engines,ISABE-2001-1223,2001.
|
| [8] |
张皓光,王云鹏,吴俊,等.组合型处理机匣提高轴流压气机稳定性的机理［J］.航空动力学报,2015,30(1):228-236.ZHANG Haoguang,WANG Yunpeng,WU Jun,et al.Mechanism of improvement on axial-flow compressor stability with assembled casing treatment［J］.Journal of Aerospace Power,2015,30(1):228-236.(in Chinese)
|
| [9] |
WILKE I,KAU H P.A numerical investigation of the flow mechanisms in a HPC front stage with axial slots［R］.ASME Paper GT2003-38481,2003.
|
| [10] |
MULLER M W.Interaction of rotor and casing treatment flow in an axial single-stage transonic compressor with circumferential grooves［R］.ASME Paper GT-2008-50135,2008.
|
| [11] |
MULLER M W.Effect of circumferential grooves on the aerodynamic performance of an axial single-stage transonic compressor［R］.ASME Paper GT2007-27365,2007.
|
| [12] |
VOGES M.Investigation of blade tip interaction with casing treatment in a transonic compressor:Part Ⅰ particle image velocimety［R］.ASME Paper GT2008-50210,2008.
|
| [13] |
VOGES M.Investigation of blade tip interaction with casing treatment in a transonic compressor:Part Ⅱ numerical results［R］.ASME Paper GT2008-50212,2008.
|
| [14] |
EMMRICH R.Time resolved investigations of an axial compressor with casing treatment:Part 1 experiment［R］.ASME Paper GT2007-27581,2007.
|
| [15] |
EMMRICH R.Time resolved investigations of an axial compressor with casing treatment:Part 2 simulation［R］.ASME Paper GT2007-27582,2007.
|
| [16] |
HALL E J,CROOK A J.Aerodynamic analysis of compressor casing treatment with a 3D Navier-Stokes solver［R］.AIAA 94-2796,1994.
|
| [17] |
HALL E J,DELANEY R A.Performance prediction of end-wall treat-fan rotors with inlet distortion［R］.AIAA 96-0244,1996.
|
| [18] |
HILA A A,OURLIDAKIS A T.Computational analysis of passive stall delay through vaned recess treatment［R］.ASME Paper 2001-GT-0342,2001.
|
| [19] |
杜辉,朱俊强,楚武利.凹槽叶片式处理机匣的结构尺寸优化研究［J］.推进技术,1998,19(1):71-75.DU Hui,ZHU Junqiang,CHU Wuli.Optimization ofstructural parameters of recess vaned casing treatment［J］.Journal of Propulsion Technology,1998,19(1):71-75.(in Chinese)
|
| [20] |
ENGEL K,ZSCHERP C,WOLFRUM N,et al.CFD simulations of the TP400 IPC with enhanced casing treatment in off-design operating conditions［R］.ASME Paper GT2009-60324,2009.
|
| [21] |
KROECKEL T,HILLER S J,ESCHKE P J.Application of a multistage casing treatment in a high speed axial compressor test rig［R］.ASME Paper GT2011-46315,2011.
|
| [22] |
楚武利,刘志伟,朱俊强.折线斜缝式处理机匣的实验研究及机理分析［J］.航空动力学报,1999,14(3):270-274.CHU Wuli,LIU Zhiwei,ZHU Junqiang.Experimental research and analysis of sloped slotted casing treatment［J］.Journal of Aerospace Power,1999,14(3):270-274.(in Chinese)
|
DownLoad: