| Citation: | SHI Pei-jie, QIAO Wei-yang, WEI Zuo-jun, XU Kun-bo. Numerical calculation model of axial compressor stability enhancement bywith discrete tip injection[J]. Journal of Aerospace Power, 2013, 28(7): 1549-1556. |
| [1] |
Pullan G,Young A M,Greitzer E M.Origins and structure of spike-type rotating stall [R].ASME Paper GT-2012-68707,2012.
|
| [2] |
Lim H S,Bae H J,Lim Y C.Injection profile effects on low speed axial compressor stability enhancement[J].Journal of Mechanical Science and Technology,2011,25(6):1501-1507.
|
| [3] |
Prince D C J,Wisler D C,Hivers D E.Study of casing treatment stall margin improvement phenomena [R].NASA CR-134552,1974.
|
| [4] |
Crook A J,Greitzer E M,Tan C S,et al.Numerical simulation of compressor endwall and casing treatment flow phenomena[J].Journal of Turbomachinery,1993,115(3):501-512.
|
| [5] |
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.
|
| [6] |
Schobeiri M T,Attia M.Active control of compressor instability and surge by stator blades adjustment[J].Journal of Propulsion and Power,2003,19(2):312-317.
|
| [7] |
Eveker K M,Gysling D L,Nett C N,et al.Integrated control of rotating stall and surge in high-speed multistage compression systems[J].Journal of Turbomachinery,1998,120(3):440-445.
|
| [8] |
Yeung S,Wang Y,Murray R M.Bleed valve rate requirements evaluation in rotating stall control on axial compressors[J].Journal of Propulsion and Power,2000,16(5):781-791.
|
| [9] |
Spakovszky Z S,Weigl H J,Paduano J D,et al.Rotating stall control in a high-speed stage with inlet distortion: Part Ⅰ radial distortion[J].Journal of Turbomachinery,1999,121(3):510-516.
|
| [10] |
Chen J P,Webster R S,Hathaway M D.Numerical simulation of stall and stall control in axial and radial compressors [R].AIAA-2006-418,2006.
|
| [11] |
Weigl H J,Paduano J D,Frechette L G.Active stabilization of rotating stall and surge in a transonic single stage axial compressor[J].Journal of Turbomachinery,1998,120(4):625-636.
|
| [12] |
Koch C C,Smith L H J.Experimental evaluation of outer casing blowing or bleeding of single stage axial flow compressor:Part 4 performance of bleed insert configuration No.3 [R].NASA CR-54590,1968.
|
| [13] |
Lee N K W,Greitzer E M.Effects of endwall suction and blowing on compressor stability enhancement[J].Journal of Turbomachinery,1990,112(1):133-144.
|
| [14] |
Suder K L,Hathaway M D,Thorp S A,et al.Compressor stability enhancement using discrete tip injection[J].Journal of Turbomachinery,2001,123(1):14-23.
|
| [15] |
Day I J.Active suppression of rotating stall and surge in axial compressors[J].Journal of Turbomachinery,1993,115(1):40-47.
|
| [16] |
Hale A,Brien W O.A three-dimensional turbine engine analysis compressor code (TEACC) for steady-state inlet distortion[J].Journal of Turbomachinery,1998,120(3):422-430.
|
| [17] |
Chima R V.A three-dimensional unsteady CFD model of compressor stability [R].NASA TM-2006-214117,2006.
|
| [18] |
Gong Y F,C S Tan,K A Gordon,et al.A computational model for short-wavelength stall inception and development in multistage compressors[J].Journal of Turbomachinery,1999,121(4):726-734.
|
| [19] |
Marble F E.Three-dimensional flow in turbomachines,aerodynamic of turbine and compressor[M].Princeton:Princeton University Press,1964.
|