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    A Probabilistic Micromechanical Code for Predicting Fatigue Life Variability: Model Development and Application 

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 004:;page 889
    Author(s): K. S. Chan; M. P. Enright
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes the development of a probabilistic micromechanical code for treating fatigue life variability resulting from material variations. Dubbed MICROFAVA (micromechanical fatigue ...
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    A New Tool for Design and Certification of Aircraft Turbine Rotors 

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 001:;page 155
    Author(s): G. R. Leverant; H. R. Millwater; R. C. McClung; M. P. Enright
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes recent enhancements to a probabilistic damage tolerance software code, DARWINTM, that can be used for design certification of aircraft jet engine titanium disks/rotors that ...
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    Probabilistic Treatment of Crack Nucleation and Growth for Gas Turbine Engine Materials 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 008:;page 82106
    Author(s): M. P. Enright; R. C. McClung; S. J. Hudak; W. L. Francis
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The empirical models commonly used for probabilistic life prediction do not provide adequate treatment of the physical parameters that characterize fatigue damage development. For these models, ...
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