论文信息 - Mistuning characteristics of a bladed rotor from a two-stage transonic compressor - 字舞流文

Mistuning characteristics of a bladed rotor from a two-stage transonic compressor

James A. Kenyon | Gregory Minkiewicz

[1] Christophe Pierre,et al. An Experimental Investigation of Vibration Localization in Bladed Disks: Part I — Free Response , 1997 .

[2] Greg Minkiewicz,et al. Dynamic Response of Low Aspect Ratio Blades in a Two Stage Transonic Compressor , 1997 .

[3] Jerry H. Griffin,et al. On Predicting the Resonant Response of Bladed Disk Assemblies , 1988 .

[4] Christophe Pierre,et al. Dynamic response of an industrial turbomachinery rotor , 1996 .

[5] A. Sinha. Calculating the statistics of forced response of a mistuned bladed disk assembly , 1986 .

[6] Robert E. Kielb,et al. Effects of Structural Coupling on Mistuned Cascade Flutter and Response , 1984 .

[7] D. S. Whitehead,et al. Effect of Mistuning on the Vibration of Turbo-Machine Blades Induced by Wakes: , 1966 .

[8] Kurt Nichol,et al. Numerical strain gage representation , 1998 .

[9] D. Ewins. Vibration Modes of Mistuned Bladed Disks , 1976 .

[10] R. C. F. Dye,et al. Vibration Amplitudes of Compressor Blades Resulting From Scatter in Blade Natural Frequencies , 1969 .

[11] A. Sinha,et al. A higher order technique to compute the statistics of forced response of a mistuned bladed disk assembly , 1989 .

[12] J. T. Wagner. Coupling of Turbomachine Blade Vibrations Through the Rotor , 1967 .

[14] Christophe Pierre,et al. A reduced-order modeling technique for mistuned bladed disks , 1994 .