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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 ...
After the relative success of Chyeranovskii's first tailless gliders and powered aircraft, the BICh-1 and BICh-2 and BICh-3, he continued the tailless theme with the BICh-5 bomber. The BICh-5 was to have been a twin-engined tailless aircraft with a retractable undercarriage, two BMW VI engines and multi segment convex elevons suspended below ...
Jarosław Naleszkiewicz's Naleszkiewicz JN-1, nicknamed Żabuś II (Froggy II; the Jach Żabuś was an earlier, unrelated Polish glider) was an experimental tailless glider which was intended to test the behaviour of a proposed twin-engined aircraft of the same configuration. It was preceded by a series of rubber-powered models which proved ...
The purpose was to investigate the future possible use of tailless and tail-first concepts. In 1944, contract Acft/3303/CB.10(c) was issued to GAL for the construction and development of four unpowered proof-of-concept aircraft, three later designated as GAL.56, plus one GAL.61.
This note was the first ever documentary evidence of an aircraft's performance written in flight by the pilot himself. [3] [4] The D.5 was subsequently certified as the first fixed-wing aircraft ever to achieve stable flight. The D.5 crashed whilst being flown by another pilot the following December, and parts of it were re-used to build the ...
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 ...
A tailless aircraft is one which has no separate horizontal stabilizer or control surface, either behind or in front of the main wing. List of aircraft Type ...