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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    Titel :

    Fatigue tests on large aircraft structures with random load sequence


    Weitere Titelangaben:

    Vermoeiingsproeven op grote vliegtuigconstructies met willekeurige belastingsvolgorde


    Beteiligte:
    Broek, D. (Autor:in)

    Erschienen in:

    Ingenieur ; 77 , n 40


    Erscheinungsdatum :

    1965


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Niederländisch


    Schlagwörter :


    Programme Load Fatigue Tests

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    Haas, T. | Engineering Index Backfile | 1955


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    Haas, Tibor | Emerald Group Publishing | 1955


    Fatigue in aircraft structures

    Barrois, W. | Engineering Index Backfile | 1955