| Citation: | Mechanism of affect on stall margin of circumferential grooves with variable pre-swirl angle[J]. Journal of Aerospace Power, 2019, 34(8): 1822-1835. doi: 10.13224/j.cnki.jasp.2019.08.023 |
| [1] |
WENNERSTROM A J.Highly loaded axial flow compressors:history and current developments[J].Journal of Turbomachinery,1990,112(4):567-578.
|
| [2] |
彭泽琰.航空燃气轮机原理[M].北京:国防工业出版社,2008:107-118.
|
| [3] |
EMMONS H W,PEARSON C E,GRANT H P.Compressor surge and stall propagation[J].Transaction of the ASME,1955,77(4):455-469.
|
| [4] |
MOORE F K.GREITZER E M.A theory of post-stall in axial flow compressors[R].Air Force Aero Propulsion Laboratory,AFAPL-TP-79-2083,1979.
|
| [5] |
INOUE M,KUROUMARU M,TANINO T,et al.Comparative studies on short and long length-scale stall cell propagatingin axial compressor rotor[J].Journal of Turbomachinery,2001,123(1):24-30.
|
| [6] |
CAMP T R,DAY I J.A study of spike and modal stall phenomena in a low- speed axial compressor[J].Journal of Turbomachinery,1998,120:393-401.
|
| [7] |
DAY I J.Stall,surge,and 75 years of research[J].Journal of Turbomachinery,2016,138:011001.1-011001.16.
|
| [8] |
SMITH G,CUMPSTY N.Flow phenomena in compressor casing treatment[J].Journal of Engineering for Gas Turbines and Power,1984,106(3):532-541.
|
| [9] |
WATERMAN M.Axial flow compressor surge margin improvement:US005137419A[P].1992-08-11.
|
| [10] |
SEITZ P.Casing treatment for axial flow compressors[D].Cambridge,US:University of Cambridge,1999.
|
| [11] |
HOUGHTON T,DAY I J.Stability enhancement by casing grooves:the importance of stall inception mechanism and solidity[R].ASME Paper GT2010-22284,2010.
|
| [12] |
GREITZER E M.Surge and rotating stall in axial flow compressors:Part Ⅰ theoretical compression system model[J].Journal of Engineering for Power,1976(98):190-217.
|
| [13] |
WILKE I,KAU H P.A numerical investigation of the influence of casing treatments on the tip leakage flow in a hpc front stage[R].ASME Paper GT2002-30642,2002.
|
| [14] |
HATHAWAY M D.Self-recirculating casing treatment concept for enhanced compressor performance[R].ASME Paper GT2002-30368,2002.
|
| [15] |
RABE D C,HAH C.Application of casing circumferential grooves for improved stall margin in a transonic axial compressor[R].ASME Paper GT-2002-30641,2002.
|
| [16] |
SHABBIR A.ADAMCZYK J J.Flow mechanism for stall margin improvement due to circumferential casing grooves on axial compressors[R].ASME Paper GT2004-53903,2004.
|
| [17] |
楚武利,张皓光,吴艳辉,等.槽式机匣槽宽变化对扩稳效果影响的试验与数值研究[J].航空学报,2015,29(4):866-872.CHU Wuli,ZHANG Haoguang,WU Yanhui,et al.Impact of Grooved Width of Grooved Casing on Stall Margin Improvement[J].Acta Aeronautica et Astronautica Sinica,2015,29(4):866-872.(in Chinese)
|
| [18] |
邓敬亮,楚武利,张皓光.轴流转子梯形周向槽处理机匣的扩稳分析[J].航空动力学报,2008,30 (7):1721-1730.DENG Jingliang,CHU Wuli,ZHANG Haoguang.Stabilizing analysis of trapezoidal circumferential grooves on an axial rotor[J].Journal of Aerospace Power,2008,30 (7):1721-1730.(in Chinese)
|
| [19] |
张皓光,安康,吴艳辉,等.周向槽轴向位置影响机匣处理扩稳能力的机理[J].推进技术,2016,37(12):2296-2302.ZHANG Haoguang,AN Kang,WU Yanhui,et al,Mechanism of affecting ability of casing treatment to improve stall margin with varying axial position of circumferential grooves[J].Journal of Propulsion Technology,2016,37(12):2296-2302.(in Chinese)
|
| [20] |
LIEBECK R H.Design of the blended-wing-body subsonic transport[J].AIAA Journal of Aircraft,2004,41(1):10-25.
|
| [21] |
ZHANG Haoguang,TAN Feng,AN Kang,et al,Numerical investigation of stall mechanism of an axial compressor at three different rotating speeds[R].ASME Paper GT2017-63777,2017.
|