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 Can Aeronautics and Space J v 13 n 8 Oct 1967 p 373-80)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Low altitude flight load spectra for light aircraft


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


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


    Erscheinungsdatum :

    1967


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Low altitude flight load spectra for light aircraft

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



    Flight simulator test of altitude-coded aircraft light

    Robinson, Jr., J.E. / Cook, K.G. | Engineering Index Backfile | 1963


    Estimation of optimal flight altitude for an aircraft

    Singh, Aman jot / Dhawan, Suvriti | AIAA | 2015