Aerodynamic effects on blade vibratory stress variations
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[1] D. S. Whitehead,et al. Effect of Mistuning on the Vibration of Turbo-Machine Blades Induced by Wakes: , 1966 .
[2] Christophe Pierre,et al. A reduced-order modeling technique for mistuned bladed disks , 1994 .
[3] Kurt Nichol,et al. Numerical strain gage representation , 1998 .
[4] R. C. F. Dye,et al. Vibration Amplitudes of Compressor Blades Resulting From Scatter in Blade Natural Frequencies , 1969 .
[5] A. Sinha,et al. A higher order technique to compute the statistics of forced response of a mistuned bladed disk assembly , 1989 .
[6] J. T. Wagner. Coupling of Turbomachine Blade Vibrations Through the Rotor , 1967 .
[7] A. Sinha. Calculating the statistics of forced response of a mistuned bladed disk assembly , 1986 .
[8] Robert E. Kielb,et al. Effects of Structural Coupling on Mistuned Cascade Flutter and Response , 1984 .
[9] D. Ewins. Vibration Modes of Mistuned Bladed Disks , 1976 .
[10] Christophe Pierre,et al. Forced response of mistuned bladed disks using reduced-order modeling , 1996 .