Results are presented of a fatigue investigation conducted using 18 outer wing panels of T-29A airplanes. Constant-amplitude tests were performed using the resonant-frequency method at three different alternating load levels superposed on a 1 g, or level-flight mean load. Information is presented concerning crack location, cycles to crack initiation, crack propagation, and residual static strength.


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    Titel :

    Fatigue Investigation of Full-Scale Wing Panels of 7075 Aluminum Alloy


    Beteiligte:
    Castle, Claude B. (Autor:in) / Ward, John F. (Autor:in)

    Erscheinungsdatum :

    01.04.1961


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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