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The effects of detuning upon the forced vibrations of bladed disks
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Consideration on the benefits of intentional blade mistuning for the forced response of turbomachinery rotors
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ASME, New York, NY
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Castanier, M. P., and Pierre, C., 1997, "Consideration on the Benefits of Intentional Blade Mistuning for the Forced Response of Turbomachinery Rotors," Analysis and Design Issues for Modern Aerospace Vehicles, ASME, New York, NY, pp. 419-425.
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Castanier, M.P.1
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Investigation of the combined effects of intentional and random mistuning on the forced response of bladed disks
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Optimization of cascade blade mistuning, part I: Equations of motion and basic inherent properties
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Optimization and mechanisms of mistuning in cascades
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IEEE, New York, NY
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Petrov, E. P., Vitali, R., and Haftka, R. T., 2000, "Optimization of Mistuned Bladed Diskcs Using Gradient-based Response Surface Approximations," AIAA Paper 2000-1552, Proceedings of the 41th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA, Reston, VA, 1, pp. 1129-1139.
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ASME, New York, NY
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Pacific Center of Thermal-Fluids Engineering, Kihei, HI
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Bladh, R., Castanier, M. P., Pierre, C., and Kruse, M. J., 2002. "Dynamic Response Predictions for a Mistuned Industrial Turbomachinery Rotor Using Reduced Order Modeling," ASME Journal of Engineering for Gas Turbines and Power, 124, pp. 311-324.
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