Mikolajczak A A.Technology status for blade flutter in axial turbomachinery[J].Journal of Fluids Engineering,1976,098:337-339
[2]
杨晓东,陶德平,周盛.对于叶轮机气动弹性力学的一个基本假设的讨论[J].中国科学A辑,1991(2):192-199 Yang Xiaodong,Tao Depin,Zhou Sheng.Discussion of a hypothesis in turbomachinery aeroelasticity[J].Science in China,1991(2):192-199(in Chinese)
[3]
张小伟,王延荣,徐可宁,叶轮机械叶片颤振的影响参数[J].航空动力学报,2011,26(7):1558-1562 Zhang Xiaowei,Wang Yanrong,Xu Kening.Effects of parameters on blade flutter in turbomachinery[J].Journal of Aerospace Power,2011,26(7):1558-1562(in Chinese)
[4]
Sadeghi M,Liu F.Coupled fluid'structure simulation for turbomachinery blade rows[R].AIAA Paper-2005-0018,2005
[5]
张小伟,王延荣.叶间相位角对叶片颤振的影响[J].航空动力学报,2010,25(2):412-416 Zhang Xiaowei,Wang Yanrong.Influence of interblade phase angle on the flutter of rotor blades[J].Journal of Aerospace Power,2010,25(2):412-416(in Chinese)
[6]
张小伟,王延荣,徐可宁,叶轮机械叶片颤振的影响参数[J].航空动力学报,2011,26(7):1558-1562 Zhang Xiaowei,Wang Yanrong,Xu Kening.Effects of parameters on blade flutter in turbomachinery[J].Journal of Aerospace Power,2011,26(7):1558-1562(in Chinese)
[7]
Bendiksen O O.A new approach to computational aeroelasticity[R].AIAA paper-1991-0939,1991
[8]
Sadeghi M,Liu F.Coupled fluid'structure simulation for turbomachinery blade rows[R].AIAA Paper-2005-0018,2005
[9]
Carta F O.Coupled blade-disk-shroud flutter instabilities in turbojet engine rotors[J].Journal of Engineering for Power,1967,89:419-426
[10]
Bendiksen O O.A new approach to computational aeroelasticity[R].AIAA paper-1991-0939,1991
[11]
Lane F.System mode shapes in the flutter of compressor blade rows[J].Journal of the Aeronautical Science,1956,23:54-66
[12]
Carta F O.Coupled blade-disk-shroud flutter instabilities in turbojet engine rotors[J].Journal of Engineering for Power,1967,89:419-426
[13]
Lane F.System mode shapes in the flutter of compressor blade rows[J].Journal of the Aeronautical Science,1956,23:54-66
[14]
张潇.基于能量法的叶片颤振边界预测方法[D].北京:北京航空航天大学,2008 Zhang Xiao.Flutter boundary prediction based on energy method[D].Beijing:Beijing Univesity of Aeronautics and Astronautics,2008(in Chinese)
[15]
He L.Method of simulating unsteady turbomachinery flows with multiple perturbations[J].AIAA Journal,1992,30(11): 2730-2735
[16]
张潇.基于能量法的叶片颤振边界预测方法[D].北京:北京航空航天大学,2008 Zhang Xiao.Flutter boundary prediction based on energy method[D].Beijing:Beijing Univesity of Aeronautics and Astronautics,2008(in Chinese)
[17]
杨青真,肖军,周新海.基于气/ 固耦合非定常流动的叶栅颤振分析[J].推进技术,2005,26(6):526-530 Yang Qingzhen,Xiao Jun,Zhou Xinhai.Cascade flutter investigation based on flow-structure coupling unsteady flow[J].Journal of Propulsion Technology,2005,26(6):526-530(in Chinese)
[18]
He L.Method of simulating unsteady turbomachinery flows with multiple perturbations[J].AIAA Journal,1992,30(11): 2730-2735
[19]
杨青真,肖军,周新海.基于气/ 固耦合非定常流动的叶栅颤振分析[J].推进技术,2005,26(6):526-530 Yang Qingzhen,Xiao Jun,Zhou Xinhai.Cascade flutter investigation based on flow-structure coupling unsteady flow[J].Journal of Propulsion Technology,2005,26(6):526-530(in Chinese)
[20]
Bréard M,Vahdati M,Sayma A I,et al.An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion[R].ASME paper-2000-GT-0373,2000
[21]
Sadeghi M,Liu F.Coupled fluid'structure simulation for turbomachinery blade rows[R].AIAA-2005-0018,2005
[22]
Zheng Yun,Yang Hui.Coupled fluid'structure flutter analysis of a transonic fan[J].Chinese Journal of Aeronautics,2011, 24(3):258-264
[23]
郑赟.基于非结构网格的气动弹性数值方法研究[J].航空动力学报,2009,24(9):2069-2077 Zheng Yun.Computational aeroelasticity with an unstructured grid method[J].Journal of Aerospace Power,2009,24(9):2069-2077(in Chinese)
[24]
张锦.叶轮机振动模态分析理论及数值方法[M].北京:国防工业出版社,2001 Zhang Jin.Theory and numerical methods for modal analysis of turbomachine vibration[M].Beijing:National Defense Industrial Press,2001(in Chinese)
[25]
张锦.叶轮机振动模态分析理论及数值方法[M].北京:国防工业出版社,2001 Zhang Jin.Theory and numerical methods for modal analysis of turbomachine vibration[M].Beijing:National Defense Industrial Press,2001(in Chinese)
[26]
Carta F O,Hilaire A O.Effect of interblade phase angle and incidence angle on cascade pitching stability[J].Journal of Engineering for Power,1980,102:391-396
[27]
杨晓东,陶德平,周盛.对于叶轮机气动弹性力学的一个基本假设的讨论[J].中国科学A辑,1991(2):192-199 Yang Xiaodong,Tao Depin,Zhou Sheng.Discussion of a hypothesis in turbomachinery aeroelasticity[J].Science in China,1991(2):192-199(in Chinese)
[28]
Srinivasan A V.Flutter and resonant vibration characteristics of engine blades[J].Journal of Engineering for Gas Turbines and Power,1997,19(4):742-775
[29]
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)
[30]
周盛.叶轮机气动弹性力学引论[M].北京:国防工业出版社,1989:3-5 Zhou Sheng.Introduction of aeroelasticity[M].Beijing:National Defense Industrial Press,1989:3-5(in Chinese)
[31]
张小伟,王延荣.叶间相位角对叶片颤振的影响[J].航空动力学报,2010,25(2):412-416 Zhang Xiaowei,Wang Yanrong.Influence of interblade phase angle on the flutter of rotor blades[J].Journal of Aerospace Power,2010,25(2):412-416(in Chinese)
[32]
Mikolajczak A A.Technology status for blade flutter in axial turbomachinery[J].Journal of Fluids Engineering,1976,098:337-339
[33]
周盛.叶轮机气动弹性力学引论[M].北京:国防工业出版社,1989:3-5 Zhou Sheng.Introduction of aeroelasticity[M].Beijing:National Defense Industrial Press,1989:3-5(in Chinese)
[34]
金琰,袁新.三维透平叶片扭转颤振问题的流固耦合数值研究[J].工程热物理学报,2004,25(1):41-44 Jin Yan,Yuan Xin.Numerical analysis of 3d turbine blade's torsional flutter by fluid'structure coupling method[J].Journal of Engineering Thermophysics,2004,25(1):41-44(in Chinese)
[35]
金琰,袁新.三维透平叶片扭转颤振问题的流固耦合数值研究[J].工程热物理学报,2004,25(1):41-44 Jin Yan,Yuan Xin.Numerical analysis of 3d turbine blade's torsional flutter by fluid'structure coupling method[J].Journal of Engineering Thermophysics,2004,25(1):41-44(in Chinese)
[36]
Johnston D A,Cross C J,Wolff J M.An architecture for fluid/structure interaction analysis of turbomachinery blading[R].AIAA-2005-4013,2005
[37]
Johnston D A,Cross C J,Wolff J M.An architecture for fluid/structure interaction analysis of turbomachinery blading[R].AIAA-2005-4013,2005
[38]
Doi H. Fluid/structure coupled aeroelastic computations for transonic flows in turbomachinery[D].Stanford:Stanford University,2002
[39]
Doi H. Fluid/structure coupled aeroelastic computations for transonic flows in turbomachinery[D].Stanford:Stanford University,2002
[40]
Bréard M,Vahdati M,Sayma A I,et al.An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion[R].ASME paper-2000-GT-0373,2000
[41]
郑赟.基于非结构网格的气动弹性数值方法研究[J].航空动力学报,2009,24(9):2069-2077 Zheng Yun.Computational aeroelasticity with an unstructured grid method[J].Journal of Aerospace Power,2009,24(9):2069-2077(in Chinese)
[42]
Sadeghi M,Liu F.Coupled fluid'structure simulation for turbomachinery blade rows[R].AIAA-2005-0018,2005
[43]
Zheng Yun,Yang Hui.Coupled fluid'structure flutter analysis of a transonic fan[J].Chinese Journal of Aeronautics,2011, 24(3):258-264
[44]
Carta F O,Hilaire A O.Effect of interblade phase angle and incidence angle on cascade pitching stability[J].Journal of Engineering for Power,1980,102:391-396
