Procedure which uses statistical methods of data analysis which provide sole means for mathematical determination of reliability from safety aspect; suggestion is made that aircraft safety should require catastrophic failure rate of less than 10-3 after 10,000 flying hours; it is shown how requirement of this type may be met, but methods are sufficiently flexible for adaptation to any requirement considered necessary in future.


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    Titel :

    Assessing helicopter safety with respect to component fatigue


    Weitere Titelangaben:

    Aircraft Eng


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

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Assessing Helicopter Safety with Respect to Component Fatigue

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


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    Comparison of Helicopter Component Fatigue Test Results to Analysis

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    3D fatigue crack propagation analysis of a helicopter component

    Colombo, Daniele / Giglio, Marco / Manes, Andrea | Tema Archiv | 2007