Maximum lift coefficient of symmetrical 10.51% thick airfoil was increased from 1.3 to approximately 1.8 by means of area suction from 0.3 to 3% chord.


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    Title :

    Effect of type of porous surface and suction velocity distribution on characteristics of 10.5-percent-thick airfoil with area suction


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1953


    Size :

    59 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :