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  2. 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.

  3. 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 ...

  4. List of tailless aircraft - Wikipedia

    en.wikipedia.org/wiki/List_of_tailless_aircraft

    A tailless aircraft is one which has no separate horizontal stabilizer or ... Research for Avro Vulcan thick delta wing, 1/3 scale of Vulcan. Avro CF-105 Arrow: Canada:

  5. Shenyang J-50 - Wikipedia

    en.wikipedia.org/wiki/Shenyang_J-50

    In 2018, Shenyang Aircraft Corporation (SAC) reportedly developed prototypes for the next-generation aircraft. [4] Intelligence and rumors indicated the Chinese designs would use tailless flying wing or flying arrowhead configuration that can provide greater broadband stealth characteristics compared to the previous generation of fighters, new propulsion technologies, improved sensors allowing ...

  6. China unveils novel advanced military aircraft - AOL

    www.aol.com/china-unveils-novel-advanced...

    The new Chinese aircraft are not the first modern tailless designs. The Northrop Grumman B-2 and B-21 stealth bombers are both flying wings, and several uncrewed aircraft, such as the Lockheed ...

  7. 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.

  8. Dunne D.7 - Wikipedia

    en.wikipedia.org/wiki/Dunne_D.7

    Data from Flight, 1911 General characteristics Crew: 1 Length: 21 ft 0 in (6.40 m) Wingspan: 36 ft 0 in (10.97 m) Wing area: 230 sq ft (21 m 2) including elevons Powerplant: 1 × Green water cooled inline, 60 hp (45 kW) Propellers: 2-bladed, 7 ft 3 in (2.21 m) diameter Notes ^ Tailless Trials ^ a b c The Dunne Monoplane, 1911 ^ Letter from Dunne to Science Museum, 20 June 1928. Archive ref. DM ...

  9. Dunne D.5 - Wikipedia

    en.wikipedia.org/wiki/Dunne_D.5

    The Dunne D.5 was a British experimental aircraft built in 1910. A tailless swept-wing biplane, it was designed by J. W. Dunne and built by Short Brothers at Leysdown for his company, the Blair Atholl Aeroplane Syndicate Ltd.