In aerodynamic sense, load factor arises when loading conditions exceed steady level flight conditions; in structural sense, aerodynamic loads cease to be ultimate and become limit loads, associated conditions being termed limit loading conditions; influence of size on load factors; effect of high (subsonic) speed; phenomena of atmospheric gusts impose loading condition and therefore load factor, in excess of initial flight condition.


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    Titel :

    Load factors in aircraft design


    Weitere Titelangaben:

    Shell Aviation News


    Beteiligte:
    Radlett, H.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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