Results of test program, undertaken at Nat Aero and Astronautical Research Inst, Amsterdam, Holland, based on gust spectrum with variable amplitude loading; validity of Palmgren-Miner rule for crack propagation is studied and its usefulness for design purposes discussed.


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    Title :

    Crack propagation


    Additional title:

    Aircraft Eng


    Contributors:
    Schijve, J. (author) / Broek, D. (author)

    Published in:

    Publication date :

    1962


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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