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  2. Leading-edge extension - Wikipedia

    en.wikipedia.org/wiki/Leading-edge_extension

    A leading-edge extension (LEX) is a small extension to an aircraft wing surface, forward of the leading edge. The primary reason for adding an extension is to improve the airflow at high angles of attack and low airspeeds, to improve handling and delay the stall. A dog tooth can also improve airflow and reduce drag at higher speeds.

  3. Westland-Hill Pterodactyl - Wikipedia

    en.wikipedia.org/wiki/Westland-Hill_Pterodactyl

    The wing was "washed out", having a slight twist which reduced the angle of incidence progressively towards the tips, providing a near-stationary overall centre of pressure and ensuring that the aircraft was stable in pitch. Thus, no horizontal stabiliser was needed and the craft was tailless, allowing the fuselage to be relatively short.

  4. Flying wing - Wikipedia

    en.wikipedia.org/wiki/Flying_wing

    The concept of the flying wing was born on 16 February 1876 when French engineers Alphonse Pénaud and Paul Gauchot filed a patent for an aero-plane or flying aircraft [5] powered by two propellers and with all the characteristics of a flying wing as we know it today. [6] Tailless aircraft have been experimented with since the earliest attempts ...

  5. Tailless aircraft - Wikipedia

    en.wikipedia.org/wiki/Tailless_aircraft

    Tailless aircraft have been flown since the pioneer days; the first stable aeroplane to fly was the tailless Dunne D.5, in 1910. The most successful tailless configuration has been the tailless delta, especially for combat aircraft, though the Concorde airliner is also a delta configuration.

  6. de Havilland DH 108 - Wikipedia

    en.wikipedia.org/wiki/De_Havilland_DH_108

    Employing the main fuselage section and engine of the de Havilland Vampire mated to a longer fuselage with a single fin and swept wings, the de Havilland DH 108 was proposed in 1944 as an aerodynamic test bed for tailless designs, particularly the DH.106 Comet which had initially been considered a tailless, swept-wing concept. [1]

  7. Category:Tailless delta-wing aircraft - Wikipedia

    en.wikipedia.org/wiki/Category:Tailless_delta...

    This page was last edited on 21 November 2015, at 19:07 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.

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  9. Category:Tailless aircraft - Wikipedia

    en.wikipedia.org/wiki/Category:Tailless_aircraft

    Tailless aircraft refers to aircraft with no distinct horizontal stabilizing surfaces in their tail section. They typically employ elevons and/or canard front stabilizing wings. These aircraft usually still have normal empennage (vertical tail fin and rudder ).