Tests were conducted on internal wings of Fokker F-27 prototype; loads applied and their sequence were based on strain gage measurements on aircraft flying in turbulent air; tests with random load sequence as well as with programmed load sequence, were carried out, both with and without ground-to-air cycles; test setup and principal results are discussed.


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    Title :

    Fatigue tests on large aircraft structures with random load sequence


    Additional title:

    Vermoeiingsproeven op grote vliegtuigconstructies met willekeurige belastingsvolgorde


    Contributors:
    Broek, D. (author)

    Published in:

    Ingenieur ; 77 , n 40


    Publication date :

    1965


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Dutch


    Keywords :


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