Analysis is presented of more than 1300-hr flight load records obtained from light aircraft engaged in low altitude terrain-following operations; it is shown that continuous operation in average low altitude environment reduces estimated fatigue life by factor of 15 to 1 when compared with normal operating environment, and in limiting condition imposed by pilot tolerance, this factor is increased to 90 to 1. (See also Canada. Nat Research Council -- Aeronautical Report LR-495 Dec 1967 39 p)


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    Titel :

    Low altitude flight load spectra for light aircraft


    Weitere Titelangaben:

    Can Aeronautics and Space J


    Beteiligte:
    Sewell, R.T. (Autor:in)


    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Low altitude flight load spectra for light aircraft

    Sewell, R.T. | Engineering Index Backfile | 1967



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