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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 ...
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.
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 ...
The chine lift increases with the square of the Mach number, helping counterbalance the rearward shift in the lift of the main wing in supersonic conditions. If a tailless (Delta) wing is trimmed for safe subsonic flight, at high speeds it gains excess trim drag in pitch and becomes excessively stable resulting in poor manoeuvrability. The ...
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.
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: