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    A Simple Model for Fatigue Crack Growth Near Stress Concentrations 

    Source: Journal of Pressure Vessel Technology:;1991:;volume( 113 ):;issue: 004:;page 542
    Author(s): R. C. McClung
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fatigue crack growth rates are often difficult to predict for short cracks growing near stress concentrations. This paper presents a simple model to predict those growth rates which incorporates ...
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    Closure and Growth of Fatigue Cracks at Notches 

    Source: Journal of Engineering Materials and Technology:;1992:;volume( 114 ):;issue: 001:;page 1
    Author(s): R. C. McClung; H. Sehitoglu
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The closure behavior of fatigue cracks growing out of notches is studied with an elastic-plastic finite element model. Crack opening stresses are shown to change significantly as the crack ...
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    Characterization of Fatigue Crack Growth in Intermediate and Large Scale Yielding 

    Source: Journal of Engineering Materials and Technology:;1991:;volume( 113 ):;issue: 001:;page 15
    Author(s): R. C. McClung; H. Sehitoglu
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Parameters previously proposed for the correlation of elastic-plastic fatigue crack growth data are critically reviewed and compared from a pragmatic engineering standpoint. Commonly employed estimates ...
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    NSTS Orbiter Auxiliary Power Unit Turbine Wheel Cracking Risk Assessment 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 302
    Author(s): T. A. Cruse; R. C. McClung; T. Y. Torng
    Publisher: The American Society of Mechanical Engineers (ASME)
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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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    Analysis of General Electric Model 7001 First-Stage Nozzle Cracking 

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 001:;page 207
    Author(s): H. L. Bernstein; J. M. Allen; R. C. McClung; T. R. Sharron
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Analyses of first-stage nozzle cracking in General Electric Model 7001B and 7001E industrial gas turbines are presented. Empirical algorithms are developed to predict the maximum extent of cracking ...
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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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