In order to construct a wind tunnel model of the symmetric NACA 642A015 airfoil profile, a Timman based airfoil transformation method was used. A smoother and tighter contour profile is obtained. The number of profile coordinates (z-plane) is brought up to 100 points, equidistantly situated on the circle contour (zeta-plane). Adjacent coordinates are calculated using Schoenberg interpolation polynomials.


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    Title :

    Conforme Afbeelding van Het Profiel NACA 642A015 (The Conformal Representation of the NACA 642A015 Profile)


    Contributors:

    Publication date :

    1984


    Size :

    51 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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