Paper examines part that metal fatigue plays in engineering of helicopter, and outlines methods used to estimate safe fatigue life of component parts of helicopter; recent flight and fatigue testing carried out at Yoevil Div of Westland Aircraft Ltd was to examine flight loading conditions upon helicopter components, which are subject to vibratory loads, and to estimate their fatigue strength; it is shown how results of tests are used in life substantiation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fatigue substantiation of helicopter components


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Hall, A.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Fatigue Substantiation of Helicopter Components

    Hall, A.D. | Emerald Group Publishing | 1963




    Fatigue Substantiation and Damage Tolerance Evaluation of Fiber Composite Helicopter Components

    Bansemir, H. / Emmerling, S. / North Atlantic Treaty Organization | British Library Conference Proceedings | 2000


    The Fatigue Substantiation of the Lynx Helicopter

    Hall, A.D. | Emerald Group Publishing | 1975