Experiments were conducted in low-speed wind tunnel to investigate the aerodynamic characteristics of an airfoil with a jet flap deflected at ninety degrees, in and out of ground effect. These tests consisted of detailed static pressure measurements on the airfoil, and helium bubble flow visualization studies of the resulting flow patterns. Substantial agreement was obtained with previous experiments conducted in England. (Modified author abstract)


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    Title :

    Experimental Investigation of Incompressible Flow Past Jet Flapped Airfoils


    Contributors:

    Publication date :

    1974


    Size :

    115 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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