| Citation: | Fan rotor blade flutter free design technology[J]. Journal of Aerospace Power, 2017, 32(7): 1718-1727. doi: 10.13224/j.cnki.jasp.2017.07.024
|
| [1] |
《航空发动机设计手册》总编委会.航空发动机设计手册：第8册 压气机［M］.北京:航空工业出版社,2000.
|
| [2] |
国际系统工程协会.系统工程手册:系统生命周期流程和活动指南［M］.张新国，译.北京:机械工业出版社,2014.
|
| [3] |
朱一凡,李群,杨峰,等.NASA系统工程手册［M］.北京:电子工业出版社,2014.
|
| [4] |
陈懋章.风扇/压气机技术发展和对今后工作的建议［J］.航空动力学报,2002,17(1):1-15.CHEN Maozhang.Development of fan/compressor techniques and suggestions on further researches［J］.Journal of Aerospace Power,2002,17(1):1-15.(in Chinese)
|
| [5] |
丁建国,胡骏.某掠型跨声风扇设计与数值模拟［J］.航空动力学报,2007,22(1):54-59.DING Jianguo,HU Jun.Design and numerical simulation of a transonic swept fan［J］.Journal of Aerospace Power, 2007,22(1):54-59.(in Chinese)
|
| [6] |
施永强.三维叶片颤振与叶片设计关联性研究［D］.西安: 西北工业大学,2006.
|
| [7] |
GILL J D,CAPECE V R.Experimental investigation of flutter in a single stage unshrouded axial-flow fan［R］.AIAA-2004-0686,2004.
|
| [8] |
REY G,BANASZUK A,GYSLING D.Active control of flutter in turbomachinery using off blade actuators sensors:experimental results［R］.AIAA-2003-1258,2003.
|
| [9] |
SIMMONS H R,BRUN K,CHERUVU S.Aerodynamic instability effects on compressor blade failure:a root cause failure analysis［R］.ASME Paper GT2006-91353,2006.
|
| [10] |
HSU K,HOYNIAK D,ANAND M S.Full-annulus multi-row flutter analyses［R］.ASME Paper GT2012-68631,2012.
|
| [11] |
刘庆瑔.发动机Ⅰ级压气机转子叶片断裂分析［J］.失效与预防,2007,2(2):34-36.LIU Qingquan.Fracture analysis on rotor blade of compressor for a series engines［J］.Failure Analysis and Prevention,2007,2(2):34-36.(in Chinese)
|
| [12] |
何凤平,张鹏峰,邵锦文.涡喷发动机压气机转子叶片的故障分析及研究［J］.战术导弹技术,2007(4):25-27.HE Fengping,ZHANG Pengfeng,SHAO Jinwen.Analysis and study of the failure of compressor rotor blade used for turbojet engine［J］.Tactical Missile Technology,2007(4):25-27.(in Chinese)
|
| [13] |
KIELB R E,KAZA K R V.Flutter of swept fan blades［R］.ASME Paper 84-GT-138,1984.
|
| [14] |
SZECHEVN F.Fan blade flutter-single blade instability or blade to blade coupling［R］.ASME Paper 85-GT-216,1985.
|
| [15] |
EL-AINI Y M.Subsonic/transonic stall flutter investigation of an advanced low pressure compressor［R］.ASME Paper 86-GT-99,1986.
|
| [16] |
PENG C.Tip running clearances effects on tip vortices induced axial compressor rotor flutter［R］.ASME Paper GT2011-45504,2011.
|
| [17] |
JOHANN E,MUCH B,NIPKAU J.Experimental and numerical flutter investigation of the 1st stage rotor in 4-stage high speed compressor［R］.ASME Paper GT2008-50698,2008.
|
| [18] |
杨晓东,侯安平,李漫露,等.相位延迟边界条件在叶轮机械颤振分析中的应用［J］.航空动力学报,2014,29(8):1846-1854.YANG Xiaodong,HOU Anping,LI Manlu,et al.Flutter analysis of turbomachinery based on phase lagged boundary condition［J］.Journal of Aerospace Power,2014,29(8):1846-1854.(in Chinese)
|
| [19] |
孙海,李坚,杨琳,等.压气机风扇叶片颤振预测和抑制的工程研究［J］.航空动力学报,2015,30(4):846-853.SUN Hai,LI Jian,YANG Lin,et al.Engineering research on prediction and suppression of blade flutter in compressor fan［J］.Journal of Aerospace Power,2015,30(4):846-853.(in Chinese)
|
| [20] |
SUN Hai,YANG Lin,LI Hongxin.Sensitive flutter parameters analysis with respect to flutter-free design of compressor blade［J］.Procedia Engineering,2015,99:39-45.
|
DownLoad: