Contains results of tunnel tests to determine effects of various combinations of split flaps, slats, and nose slats on the stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow.


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    Title :

    The Effects of High-lift Devices on the Low-speed Stability of a Tapered 37.5 Degree Sweptback Wing of Aspect Ratio 3 in Straight and Rolling Flow


    Contributors:

    Publication date :

    1948-11-09


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English