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    Discussion: “Corner Crack at the Bore of a Rotating Disk” (Kobayashi, A. S., Polvanich, N., Emery, A. F., and Love, W. J., 1976, ASME J. Eng. Power, 98, pp. 465–470) 

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004:;page 470
    Author(s): T. A. Cruse
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Erratum: “Low Cycle Fatigue Life Model for Gas Turbine Engine Disks” (Journal of Engineering Materials and Technology, 1980, 102, pp. 45–49) 

    Source: Journal of Engineering Materials and Technology:;1980:;volume( 102 ):;issue: 002:;page 199
    Author(s): T. G. Meyer; T. A. Cruse
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Low Cycle Fatigue Life Model for Gas Turbine Engine Disks 

    Source: Journal of Engineering Materials and Technology:;1980:;volume( 102 ):;issue: 001:;page 45
    Author(s): T. G. Meyer; T. A. Cruse
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A low cycle fatigue (LCF) life exhaustion method is developed for gas turbine engine disks subjected to complex mission history loading. The method is incorporated into an algorithm for LCF ...
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    Probabilistic Mesomechanical Fatigue Crack Nucleation Model 

    Source: Journal of Engineering Materials and Technology:;1997:;volume( 119 ):;issue: 001:;page 65
    Author(s): R. G. Tryon; T. A. Cruse
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A probabilistic mesomechanical crack nucleation model is proposed to link the microstructural material heterogeneities to the statistical scatter in the macro structural response. The macrostructure ...
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    A Cumulative Fatigue Damage Model for Gas Turbine Engine Disks Subjected to Complex Mission Loading 

    Source: Journal of Engineering for Gas Turbines and Power:;1979:;volume( 101 ):;issue: 004:;page 563
    Author(s): T. A. Cruse; T. G. Meyer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of a continuing research program is to develop a low cycle fatigue (LCF) damage model which accurately evaluates the life exhaustion of military gas turbine engine disks subjected ...
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    The Boundary Element Method 

    Source: Journal of Applied Mechanics:;1979:;volume( 046 ):;issue: 003:;page 718
    Author(s): C. A. Brebbia; T. A. Cruse
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Shear Strength of a Thermal Barrier Coating Parallel to the Bond Coat 

    Source: Journal of Engineering Materials and Technology:;1998:;volume( 120 ):;issue: 001:;page 26
    Author(s): T. A. Cruse; R. C. Dommarco; P. C. Bastías
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The static and low cycle fatigue strength of an air plasma sprayed (APS) partially stabilized zirconia thermal barrier coating (TBC) is experimentally evaluated. The shear testing utilized the ...
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    Integral Equation Methods in Potential Theory and Elastostatics 

    Source: Journal of Applied Mechanics:;1978:;volume( 045 ):;issue: 004:;page 966
    Author(s): M. A. Jaswon; T. A. Cruse; G. T. Symm
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Thermal Barrier Coating Life Prediction Model Development 

    Source: Journal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 004:;page 610
    Author(s): T. A. Cruse; M. Ortiz; S. E. Stewart
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Ceramic thermal barrier coating tests show that the coating fails by ceramic spallation. Analysis of life data indicates that cyclic thermal loading and thermal exposure play synergistic roles ...
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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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