| Citation: | XIE Fang, CHU Wu-li, LI Xiang-jun, LIU Chuan-le. Influence of blade tip clearance at near-stall condition on transonic axial-flow compressor[J]. Journal of Aerospace Power, 2014, (10): 2417-2423. doi: 10.13224/j.cnki.jasp.2014.10.019
|
| [1] |
邹正平,李宇,刘火星,等.民用大涵道比涡扇发动机叶轮机某些关键技术[J].航空动力学报,2008,23(8):1504-1518. ZOU Zhengping,LI Yu,LIU Huoxing,et al.Key turbomachinery technology of civil high-bypass-ratio turbofan engine[J].Journal of Aerospace Power,2008,23(8):1504-1518.(in Chinese)
|
| [2] |
DeCastro J A,Melcher K M.A study on the requmements for first active turbine tip clearance control[R].AIAA-2004-4176,2004.
|
| [3] |
Stinetz B M,Lattime S B,Taylor S,et al.Evaluation of an active clearance control system concept[R].AIAA-2005-3989,2005.
|
| [4] |
曾军,王鹏飞.民用航空发动机涡轮叶尖间隙主动控制技术分析[J].航空科学技术,2012,6(2):1-6. ZENG Jun,WANG Pengfei.Analysis on turbine active clearance control technology of civil aircraft engine[J].Aeronautical Science & Technology,2012,6(2):1-6.(in Chinese)
|
| [5] |
Smith G D J,Cumpsty N A.Flow phenonmena in compressor casing treament[J].Engineer for Gas Turbines and Power,1984,106(7):532-541.
|
| [6] |
Yamada K,Funazaki K,Furukawa M.Behavior of tip clearance flow at near-stall condition in a transonic axial compressor rotor[R].ASME Paper 2007-GT-27725,2007.
|
| [7] |
杜鹃,林峰,张宏武,等.跨音速轴流压气机风扇转子叶尖泄漏流的数值研究[J].工程热物理学报,2008,29(12):2027-2032. DU Juan,LIN Feng,ZHANG Hongwu,et al.Numerical simulation on unsteady tip leakage flow in a transonic axial fan rotor[J].Journal of Engineering Thermophysics,2008,29(12):2027-2032.(in Chinese)
|
| [8] |
Schlechtriem S,Lotzerich M.Breakdown of tip leakage vortices in compressors at flow conditions close to stall[R].ASME Paper 1997-GT-41,1997.
|
| [9] |
Reid L,Moore 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.
|
| [10] |
卢新根.轴流压气机内部流动失稳及其被动控制策略研究[D].西安:西北工业大学,2007. LU Xingen.Flow instability and its passive control strate-gies in axial-flow compressor[D].Xi'an:Northwestern Polytechnical University,2007.(in Chinese)
|
| [11] |
谢芳,楚武利,张皓光.跨声速轴流压气机激波/泄漏涡/边界层分离相互作用的影响[J].航空动力学报,2012,27(2):425-430. XIE Fang,CHU Wuli,ZHANG Haoguan.Influence shock waves leakage vortex boundary layer separation interaction in a single-stage transonic axial compressor[J].Journal of Aerospace Power,2012,27(2):425-430.(in Chinese)
|
| [12] |
Suder K L,Celestina M L.Experiment and computational investigation of the tip clearance flow in a transonic axial compressor rotor[R].NASA Technical Memorandum 106711,1994.
|
| [13] |
Wilke I,Kau H P.A numerical of the influence of casing treatment on the tip leakerage flow in a HPC front stage[R].ASME Paper 2002-GT-30642,2002.
|
| [14] |
吴介之,马晖扬,周明德.涡动力引论[M].北京:高等教育出版社,1993.
|
| [15] |
童秉纲.非定常流与涡运动[M].北京:国防工业出版社,1993.
|
| [16] |
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. ZHANG Yanfeng.Investigation of endwall flow behaviour and its control strategies in highly loaded compressor[D].Xi'an:Northwestern Polytechnical University,2010.(in Chinese)
|
| [17] |
李相君,楚武利,张皓光,等.高负荷跨音速轴流压气机的叶型优化设计[J].计算机仿真,2012,29(7):75-79. LI Xiangjun,CHU Wuli,ZHANG Haoguang,et al.Optimization design for high loading transonic axial compressor blade profile[J].Computer Simulation,2012,29(7):75-79.(in Chinese)
|
| [18] |
夏钦斌,王如根,周敏,等.低雷诺数条件下跨声速转子轴向倾斜缝处理机匣扩稳研究[J].航空动力学报,2010,25(6):1389-1393. XIA Qinbin,WANG Rugen,ZHOU Min,et al.Research on the effects of a transonic compressor rotor with axial skewed slots casing treatment at low Reynolds[J].Journal of Aerospace Power,2010,25(6):1389-1393.(in Chinese)
|
DownLoad: