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    Experimental Demonstration of Maximum Mistuned Bladed Disk Forced Response 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 004:;page 673
    Author(s): J. A. Kenyon; J. H. Griffin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theory was previously developed for predicting robust maximum forced response in mistuned bladed disks from distortion of a structural mode. This paper describes an experiment to demonstrate ...
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    Forced Response of Turbine Engine Bladed Disks and Sensitivity to Harmonic Mistuning 

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001:;page 113
    Author(s): J. A. Kenyon; J. H. Griffin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The mistuned forced response of turbine engine bladed disks is treated using harmonic perturbations in the properties of a continuous ring. A continuous shear spring is attached to the ring ...
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    Maximum Bladed Disk Forced Response From Distortion of a Structural Mode 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002:;page 352
    Author(s): J. A. Kenyon; J. H. Griffin; D. M. Feiner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method is presented for obtaining maximum bladed disk forced response from distortion of a structural mode. It is shown that maximum response from mode distortion in a bladed disk occurs ...
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    Sensitivity of Tuned Bladed Disk Response to Frequency Veering 

    Source: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 004:;page 835
    Author(s): J. A. Kenyon; J. H. Griffin; N. E. Kim
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A continuous method is presented for representing the mode interaction that occurs in frequency veering in terms of the nominal sector modes of a cyclic symmetric bladed disk model constrained ...
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