We shall attempt here to summarize the existing data on the values of the low-speed CLmax. of wings, in the absence of a fuselage, and without including information on stalling incidence or pitching moment. The summary is limited to the consideration of unswept wings, and those of delta plan form, which have symmetrical sections: there is some discussion of the maximum lift increments due to the use of flaps of various kinds.


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    Titel :

    Maximum Lift Data for Symmetrical Wings


    Untertitel :

    A Resumé of Maximum Lift Data for Symmetrical Wings, including various High-Lift Aids


    Beteiligte:
    Nonweiler, T. (Autor:in)


    Erscheinungsdatum :

    1955-01-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Maximum lift data for symmetrical wings

    Nonweiler, T. | Engineering Index Backfile | 1955


    Maximum lift prediction for multielement wings

    VALAREZO, WALTER / CHIN, VINCENT | AIAA | 1992




    Investigation of maximum lift of wings at supersonic speeds

    Gallagher, J.J. / Mueller, J.N. | Engineering Index Backfile | 1955