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  2. Flap (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Flap_(aeronautics)

    A flap is a high-lift device used to reduce the stalling speed of an aircraft wing at a given weight. Flaps are usually mounted on the wing trailing edges of a fixed-wing aircraft. Flaps are used to reduce the take-off distance and the landing distance. Flaps also cause an increase in drag so they are retracted when not needed.

  3. Gouge flap - Wikipedia

    en.wikipedia.org/wiki/Gouge_flap

    The Gouge flap, is a type of aircraft flap, which moves on a track when raised or lowered; in level flight. Invented by Arthur Gouge of Short Brothers in 1936, it allows pilots to increase both the wing area and the chord of an aircraft's wing, thereby reducing the stalling speed at a given weight. This provides benefits including a shorter ...

  4. Aircraft fairing - Wikipedia

    en.wikipedia.org/wiki/Aircraft_fairing

    The wing root fairing of an American Aviation AA-1 Yankee. An aircraft fairing is a structure whose primary function is to produce a smooth outline and reduce drag. [1]These structures are covers for gaps and spaces between parts of an aircraft to reduce form drag and interference drag, and to improve appearance.

  5. Trim tab - Wikipedia

    en.wikipedia.org/wiki/Trim_tab

    Typical trim tabs on aileron, rudder and elevator. Trim tabs are small surfaces connected to the trailing edge of a larger control surface on a boat or aircraft, used to control the trim of the controls, i.e. to counteract hydro- or aerodynamic forces and stabilise the boat or aircraft in a particular desired attitude without the need for the operator to constantly apply a control force.

  6. Gurney flap - Wikipedia

    en.wikipedia.org/wiki/Gurney_flap

    A net benefit in overall lift-to-drag ratio is possible if the flap is sized appropriately, based on the boundary layer thickness. [23] The Gurney flap increases lift by altering the Kutta condition at the trailing edge. [5] [9] The wake behind the flap is a pair of counter-rotating vortices that are alternately shed in a von Kármán vortex ...

  7. Leading-edge droop flap - Wikipedia

    en.wikipedia.org/wiki/Leading-edge_droop_flap

    Droop flaps function with other high-lift devices on an aircraft to increase the camber of the wing and reduce the stalling speed.On the Airbus A380, the first stage of lift device selection deploys the droop flaps (called droop noses by Airbus) and leading-edge slats located further out on the wing; with the main flaps starting to extend when the second stage is selected.

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