[1]Wei S T,Pierre C. Localization Phenomena in Mistuned Assemblies with Cyclic Symmetry, Part 1:Free Vibrations [J]. ASME, Journal of Vibration, Acoustics, Stress, and Reliability in Design, 1988,110 : 429-438.
[2]Bladeh R, Castanier M P, Pierre C. Reduced Order Modeling and Vibration Analysis of Mistuned Bladed Disk Assemblies with Shrouds[J]. Journal of Engineering for Gas Turbines and Power, 1999, 121 (3): 515- 522.
[3]周传月,邹经湘.失调对叶片—轮盘耦合系统振动影响的预测[J].航空学报,2001,22(5):465-467.
[4]王建军,李其汉,等.失谐叶片—轮盘结构系统振动局部化问题的研究进展[J].力学进展,2000,30(4):517-528.
[5]Bernstein H L, Alien J M. Analysis of Cracked Gas Turbine Blades[J]. Journal of Engineering for Gas Turbines and Power, 1992,114(2) : 293-301.
[6]Walls D P,Delaneuville R E,Cunningham S E. Damage Tolerance Based Life Prediction in Gas Turbine Engine Blades under Vibratory High Cycle Fatigue[J]. Journal of Engineering for Gas Turbines and Power, 1997,119 (1) :143-146.
[7]Wicks B J, Antoniou R A. An Investigation of Fatigue Failures of Turbine Blades in a Gas Turbine Engine by Mechanical Analysis[J]. Engineering Failure Analysis, 2002,9(2) :201-211.
[8]Wauer J. Dynamics of Cracked Rotating Blades[J]. Applied Mechanics Reviews, 1991,44(11):273-278.
[9]Dimarogonas A D. Vibration of Cracked Structures: A State of Art Review[J]. Engineering Fracture Mechanics,1996,55(5) : 831-857.
[10]Fang X,Tang J. Crack Induced Vibration Localization in Simplified Bladed-disk Structures[J]. Journal of Sound and Vibration,2006,291(2):395-418.
[11]Hou J F. Cracking Induced Mistuning in Blade Disks [J]. AIAA Journal, 2006,44 (11) : 2542-2546.
[12]王红建.复杂耦合失谐叶片—轮盘系统振动局部化问题研究[D].西北工业大学,2006:
[13]邢德顺.带单侧裂纹楔梁动力特性研究[J].航空动力学报,1999,14(4):371-374. |