Concept of "sharp edged" gust in which wing is assumed to obey laws of steady flow has proved useful as temporary expedient in setting up design criteria for gust loads; however, trend toward construction of large, heavily loaded transport airplanes and problem, of light airplane require further rationalization of these criteria. (see also Aircraft Eng v 9 n 102 Aug 1937 p 212-8)


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    Titel :

    Gust loads on airplanes


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Rhode, R.V. (Autor:in)


    Erscheinungsdatum :

    1937


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Gust loads on airplanes

    Rhode, R.V. | Engineering Index Backfile | 1937


    Gust Loads on Airplanes

    Rhode, Richard V. | SAE Technical Papers | 1937


    Calculated gust loads for tailless airplanes

    Anderson, R.F. | Engineering Index Backfile | 1945


    Gust loads on rigid airplanes with pitching neglected

    Bisplinghoff, R.L. / Isakson, G. / O'Brien, T.F. | Engineering Index Backfile | 1951


    Summary of information relating to gust loads on airplanes

    Donely, P. | Engineering Index Backfile | 1950