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  2. NACA airfoil - Wikipedia

    en.wikipedia.org/wiki/NACA_airfoil

    A new approach to airfoil design was pioneered in the 1930s, in which the airfoil shape was mathematically derived from the desired lift characteristics. Prior to this, airfoil shapes were first created and then had their characteristics measured in a wind tunnel. The 1-series airfoils are described by five digits in the following sequence:

  3. National Advisory Committee for Aeronautics - Wikipedia

    en.wikipedia.org/wiki/National_Advisory...

    NACA experience provided a model for World War II research, the postwar government laboratories, and NACA's successor, the National Aeronautics and Space Administration (NASA). NACA also participated in development of the first aircraft to fly to the "edge of space", North American's X-15. NACA airfoils are still used on modern aircraft.

  4. NACA duct - Wikipedia

    en.wikipedia.org/wiki/NACA_duct

    The Ferrari F40 sports car has "NACA style" side and hood scoops.. It is especially favored in racing car design. [4] [5] Sports cars featuring prominent NACA ducts include the Ferrari F40, the Lamborghini Countach, the 1996–2002 Dodge Viper, the 1971–1973 Ford Mustang, the 1973 Pontiac GTO, the 1979 Porsche 924 Turbo, the Maserati Biturbo, the Nissan S130, and the Porsche 911 GT2.

  5. File:Airfoil geometry.svg - Wikipedia

    en.wikipedia.org/wiki/File:Airfoil_geometry.svg

    This work has been released into the public domain by its author, F l a n k e r.This applies worldwide. In some countries this may not be legally possible; if so: F l a n k e r grants anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law.

  6. Drag curve - Wikipedia

    en.wikipedia.org/wiki/Drag_curve

    Drag and lift coefficients for the NACA 63 3 618 airfoil. Full curves are lift, dashed drag; red curves have R e = 3·10 6, blue 9·10 6. Coefficients of lift and drag against angle of attack. Curve showing induced drag, parasitic drag and total drag as a function of airspeed. Drag curve for the NACA 63 3 618 airfoil, colour-coded as opposite plot.

  7. Airfoil - Wikipedia

    en.wikipedia.org/wiki/Airfoil

    Some important parameters to describe an airfoil's shape are its camber and its thickness. For example, an airfoil of the NACA 4-digit series such as the NACA 2415 (to be read as 2 – 4 – 15) describes an airfoil with a camber of 0.02 chord located at 0.40 chord, with 0.15 chord of maximum thickness.

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  9. File:NACA 0006.svg - Wikipedia

    en.wikipedia.org/wiki/File:NACA_0006.svg

    NACA 0006, airfoil; Profil: Source: Own work: Author: ILA-boy: Licensing. Public domain Public domain false false: I, the copyright holder of this work, release this ...