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    Titel :

    Fatigue Tolerant Design in Airframes and the Influence of Vibration Suppression on Crack Growth in Helicopters



    Kongress:

    23rd:; Symposium, International Committee on Aeronautical Fatigue; ICAF 2005: structural integrity of advanced aircraft and life extension for current fleets: lessons learned in 50 years after the Comet accidents ; 2005 ; Hamburg, Germany



    Erscheinungsdatum :

    2005-01-01


    Format / Umfang :

    12 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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