Comparisons of Analytical Crack Closure Models and Experimental Results Under Flight Spectrum Loading

    Volume 1, Issue 8 (September 2004)

    ISSN: 1546-962X

    CODEN: JAIOAD

    Published Online: 30 August 2004

    Page Count: 21


    McClung, RC
    Senior Program Manager, Senior Research Engineer, and Research Engineer, Southwest Research Institute, San Antonio, TX

    McMaster, FJ
    Senior Program Manager, Senior Research Engineer, and Research Engineer, Southwest Research Institute, San Antonio, TX

    Feiger, JH
    Senior Program Manager, Senior Research Engineer, and Research Engineer, Southwest Research Institute, San Antonio, TX

    (Received 29 May 2002; accepted 17 July 2003)

    Abstract

    Spectrum FCG data were generated with corner cracks at center holes for three contrasting spectrum types and two aluminum alloys, 2124-T851 and 7475-T7351. Existing strip-yield crack closure models for FCG analysis under spectrum loading were evaluated in comparison to conventional FCG models and enhanced as needed. Spectrum editing methods based on closure behavior were developed to reduce both computational and experimental time. FASTRAN was modified to address apparent differences in closure behavior between the surface and bore tips for compression-dominated spectra. Strip yield models successfully predicted FCG lives for contrasting spectra with a common constraint factor, unlike conventional models.


    Paper ID: JAI19041

    DOI: 10.1520/JAI19041

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    Author
    Title Comparisons of Analytical Crack Closure Models and Experimental Results Under Flight Spectrum Loading
    Symposium Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions, 2002-05-31
    Committee E08