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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    Title :

    Maximum Lift Data for Symmetrical Wings


    Subtitle :

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


    Contributors:


    Publication date :

    1955-01-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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