Tests made by de Havilland Aircraft Co; wing sustained repeated applications of different loadings between 1.5g and 4.37g, particular interest being focused on Redux joints between skin and stringers; fin sustained 60,000 cycles in reversal of 33% of fully factored load and 30 cycles in reversal of 66.7%.


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    Title :

    Repeated loading and fatigue tests on D.H. 104 (Dove) wing and fin


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1950


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Repeated Loading and Fatigue Tests on a D.H. 104 (Dove) Wing and Fin

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