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  2. NACA airfoil - Wikipedia

    en.wikipedia.org/wiki/NACA_airfoil

    A: blue line = chord, green line = camber mean-line, B: leading-edge radius, C: xy coordinates for the profile geometry (chord = x axis; y axis line on that leading edge) The NACA airfoil series is a set of standardized airfoil shapes developed by this agency, which became widely used in the design of aircraft wings.

  3. Airfoil - Wikipedia

    en.wikipedia.org/wiki/Airfoil

    An airfoil (American English) or aerofoil (British English) is a streamlined body that is capable of generating significantly more lift than drag. [1] Wings, sails and propeller blades are examples of airfoils. Foils of similar function designed with water as the working fluid are called hydrofoils.

  4. Clark Y airfoil - Wikipedia

    en.wikipedia.org/wiki/Clark_Y_airfoil

    Clark Y is the name of a particular airfoil profile, widely used in general purpose aircraft designs, and much studied in aerodynamics over the years. The profile was designed in 1922 by Virginius E. Clark using thickness distribution of the German-developed Goettingen 398 airfoil. [1]

  5. Kline–Fogleman airfoil - Wikipedia

    en.wikipedia.org/wiki/Kline–Fogleman_airfoil

    Aircraft wing showing the KFm3 Step. The Kline–Fogleman airfoil or KF airfoil is a simple airfoil design with single or multiple steps along the length of the wing. It was originally devised in the 1960s for paper airplanes. In the 21st century the KF airfoil has found renewed interest among hobbyist builders of radio-controlled aircraft, due ...

  6. Aerodynamic center - Wikipedia

    en.wikipedia.org/wiki/Aerodynamic_center

    The aerodynamic center is the point at which the pitching moment coefficient for the airfoil does not vary with lift coefficient (i.e. angle of attack), making analysis simpler. [1] where is the aircraft lift coefficient. The lift and drag forces can be applied at a single point, the center of pressure. However, the location of the center of ...

  7. Wright Flyer - Wikipedia

    en.wikipedia.org/wiki/Wright_Flyer

    The Wright Flyer was a canard biplane configuration, with a wingspan of 40 feet 4 inches (12.29 m), a camber of 1-20, a wing area of 510 square feet (47 m 2), and a length of 21 feet 1 inch (6.43 m). The right wing was 4 inches (10 cm) longer because the engine was 30 to 40 pounds (14 to 18 kg) heavier than Orville or Wilbur.

  8. Leading-edge slot - Wikipedia

    en.wikipedia.org/wiki/Leading-edge_slot

    Leading-edge slot. A leading-edge slot is a fixed aerodynamic feature of the wing of some aircraft to reduce the stall speed and promote good low-speed handling qualities. A leading-edge slot is a spanwise gap in each wing, allowing air to flow from below the wing to its upper surface. In this manner they allow flight at higher angles of attack ...

  9. Template:Aircraft specifications/doc - Wikipedia

    en.wikipedia.org/wiki/Template:Aircraft...

    The model of jet or rocket used by the aircraft. The configuration of jet, such as turbojet, turbofan, motorjet, rocket, etc. Thrust of the engine with afterburner, if applicable. The thrust of the engine; if the engine has afterburners, this parameter denotes dry thrust.

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