The aerodynamic characteristics of several supercritical airfoils interim to the improved 10-percent thick NASA supercritical airfoil 26a are discussed. The airfoils have related slope and curvature distributions over the rear which result in different aft camber. For identification, the airfoils are designated supercritical airfoils 12, 13, 21, 22, and 24. Data is presented without analysis.


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    Title :

    Aerodynamic Characteristics of 10 Percent Thick NASA Supercritical Airfoils with Different Aft Camber


    Contributors:

    Publication date :

    1975


    Size :

    192 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English