Load environments for general aviation and business aircraft have not been matter of concern in past, except for static strength purposes; increased recognition of importance of fatigue qualification must be accompanied by examination of how these aircraft are being used; approach suggested by Lear Jet Corp is simplification of that used by transport aircraft industry; examinations of gust and maneuver load environments are made relative to different types of flight operations; ground-air-ground cycles, cabin pressurization, and landing load experiences are also examined.


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    Titel :

    Defining fatigue load environment for business aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Thompson, C.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1966



    Erscheinungsdatum :

    1966


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Defining the Fatigue Load Environment for Business Aircraft

    Thompson, Claude M. | SAE Technical Papers | 1966


    Modeling of the Aircraft Fatigue Load Environment

    Arrieta, A. / Striz, A. / AIAA | British Library Conference Proceedings | 2000


    Modeling of the aircraft fatigue load environment

    Arrieta, Albert / Striz, Alfred | AIAA | 2000


    Fatigue load monitoring of military aircraft

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1970