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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    Titel :

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


    Beteiligte:
    J. J. H. Blom (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    51 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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