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  • Theoretical and experimental study of a zero torgue coefficient wing section.

    T.E.I. of Crete, School of Engineering (STEF), Department of Mechanical Engineering
    Authors: Totozani, Emilnta Aimilia
    Thesis advisor: Christakis, Dimitrios
    Publication Date: 07-10-2014
    The NACA 662 215 airfoil is tested in a small wind tunnel and the measurements are compared with numerical calculations. All the three coefficients, CL , CD , Cm are compared with the NACA coefficients as they are edited ...