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  2. Vortex generator - Wikipedia

    en.wikipedia.org/wiki/Vortex_generator

    The Symphony SA-160 was designed with two unusual vortex generators on its wing to ensure aileron effectiveness through the stall. A vortex generator (VG) is an aerodynamic device, consisting of a small vane usually attached to a lifting surface (or airfoil, such as an aircraft wing) [1] or a rotor blade of a wind turbine. [2]

  3. Strake (aeronautics) - Wikipedia

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

    Nose, wing and ventral strakes Vortices over the wing strakes of an F/A-18E Super Hornet. In aviation, a strake is an aerodynamic surface generally mounted on the fuselage of an aircraft to improve the flight characteristics either by controlling the airflow (acting as large vortex generators) or by a simple stabilising effect.

  4. Vortex lift - Wikipedia

    en.wikipedia.org/wiki/Vortex_lift

    Wings which generate vortex lift have been used on delta-winged research aircraft such as the Convair XF-92A and Fairey Delta 2. Early delta wing fighters such as the F-102 , the F-106 , and contemporaries such as Dassault's deltas had cambered leading edges that were blunt and did not generate significant vortexes.

  5. Vortilon - Wikipedia

    en.wikipedia.org/wiki/Vortilon

    When the speed is reduced and the aircraft approaches stall, the local flow at the leading edge is diverted outwards; this spanwise component of velocity around the vortilon creates a vortex streamed around the top surface, which energises the boundary layer. [6] A more turbulent boundary layer, in turn, delays the local flow separation.

  6. Wing configuration - Wikipedia

    en.wikipedia.org/wiki/Wing_configuration

    Vortex devices. Vortex devices maintain airflow at low speeds and delay the stall, by creating a vortex which re-energises the boundary layer close to the wing. Vortex generator: small triangular protrusion on the upper leading wing surface; usually, several are spaced along the span of the wing. Vortex generators create additional drag at all ...

  7. Cessna 402 - Wikipedia

    en.wikipedia.org/wiki/Cessna_402

    The Cessna 402C may be outfitted with vortex generators to increase maximum allowable takeoff weight to 7,210 lb (3,270 kg), with a zero-fuel weight of 6,750 lb (3,062 kg). [ 7 ] Another modification for the 402C increases the maximum landing weight to 7,200 lb (3,266 kg), which allows commercial operators to fly with an increased payload on ...

  8. Wingtip vortices - Wikipedia

    en.wikipedia.org/wiki/Wingtip_vortices

    The intensity or strength of the vortex is a function of aircraft size, speed, and configuration (flap setting, etc.). The strongest vortices are produced by heavy aircraft, flying slowly, with wing flaps and landing gear retracted ("heavy, slow and clean"). [ 10 ]

  9. Wing fence - Wikipedia

    en.wikipedia.org/wiki/Wing_fence

    By obstructing span-wise airflow along the wing, they prevent the entire wing from stalling at once, as opposed to wingtip devices, which increase aerodynamic efficiency by seeking to recover wing vortex energy. As a swept-wing aircraft slows toward the stall speed of the wing, the angle of the leading edge forces some of the airflow sidewise ...