The purpose of the work described is to evaluate the use of acoustic emission (AE) methods to detect fatigue crack growth in aircraft structure during operation. A unique AE monitor system installed on an Australian Air Force Macchi 326 aircraft has detected AE which correlates with slow crack growth during operation over the past year and a half.


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    Titel :

    In-flight fatigue crack monitoring using acoustic emission


    Weitere Titelangaben:

    Ermuedungsbruch-Ueberwachung waehrend des Fluges mit Hilfe der akustischen Emission


    Beteiligte:
    Hutton, P.H. (Autor:in) / Skorpik, J.R. (Autor:in)

    Erschienen in:

    ISA Transactions ; 20 , 1 ; 79-83


    Erscheinungsdatum :

    1981


    Format / Umfang :

    5 Seiten, 11 Bilder


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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