Constant amplitude fatigue tests of 72 P-51D "Mustang" wings performed by vibrational loading system and by hydraulic loading device for conditions with and without varying amounts of preload. Originally issued as Report ARL/SM 207, Aeronautical Research Laboratories, Australia.


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    Title :

    Interim report on fatigue characteristics of typical metal wing


    Additional title:

    NACA -- Tech Memo


    Contributors:
    Kepert, J.L. (author) / Payne, A.O. (author)


    Publication date :

    1956


    Size :

    80 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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