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NACA 0015 TAPED AIRFOIL

NACA 0015 TAPED AIRFOIL

grabcad

These are files used for fluid simulation to determinate the lift and drag coefficients of the Airfoil NACA 0015.There is the NACA 0015 model and the Boundaries Model.The Boundary Model it is in distinct angles of attack, as 0º, 2º, 4º, 6º, 8º, 10º, 12º, 14º, 16º, 18º, 20º, 22º and 24º

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