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Sunday, February 14, 2016

Angielski samolot mysliwski WESTLAND WHIRLWIND

Westland Whirlwind Papercraft

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The Westland Whirlwind was a British twin-engined heavy fighter developed by Westland Aircraft. A contemporary of the Supermarine Spitfire and Hawker Hurricane, it was the Royal Air Force's first single-seat, twin-engined, cannon-armed fighter. When it first flew in 1938, the Whirlwind was one of the fastest and most heavily-armed combat aircraft in the world. Protracted development problems with its Rolls-Royce Peregrine engines delayed the project and only a relatively small number of Whirlwinds were built. During the Second World War, only three RAF squadrons were equipped with the Whirlwind, and despite its successful use as a fighter and ground attack aircraft it was withdrawn from service in 1943. Design and development Westland Whirlwind prototype L6845 c. 1940
By the mid-1930s, aircraft designers around the world perceived that increased attack speeds were imposing shorter firing times on fighter pilots. However, the weight of ammunition delivered could also be increased. Instead of two rifle-calibre machine guns, six or eight were required; studies had shown that eight machine guns could deliver 256 rounds per second.[1] Cannon, such as the French 20mm Hispano-Suiza HS.404, which could fire explosive ammunition, offered another type of heavy firepower and attention turned to aircraft designs which could carry four cannon. While the most agile fighter aircraft were generally small and light, their limited fuel storage also limited their range and tended to restrict them to defensive and interception roles. The larger airframes and bigger fuel loads of twin-engined designs were therefore favoured for long-range, offensive roles. The first British specification for a high performance machine-gun monoplane was F.5/34, but the aircraft produced were overtaken by developments by Hawker and Supermarine.[2] The RAF Air Staff thought that an experimental aircraft armed with the 20mm cannon was needed urgently and Air Ministry specification F.37/35 was issued in 1935. The specification called for a single-seat day and night fighter armed with four cannon. The top speed had to be at least 40 mph (64 km/h) greater than that of contemporary bombers – at least 330 mph (530 km/h) at 15,000 ft (4,570 m).
Eight aircraft designs from five companies were submitted in response to the specification. Boulton Paul offered the P.88A and P.88B (two related single engine designs); Bristol the single-engined Type 153 and the twin-engined Type 153A; Hawker offered a variant of the Hurricane; the Supermarine 312 was a variant of Spitfire and the Supermarine 313 a twin engined design with four guns in the nose and potentially a further two firing through the propeller hubs; the Westland P.9 had two Rolls-Royce Kestrel K.26 engines and a twin tail.[3][4] When the designs were considered in May 1936, there were two issues – concern that two engines would be less manoeuvrable than a single-engined design and that uneven recoil from cannon set in the wings would give less accurate fire. The conference favoured two engines with the cannon set in the nose and recommended the Supermarine 313.[5] Although Supermarine's efforts were favoured due to their previous success with fast aircraft and the promise of the Spitfire which was undergoing trials, neither they nor Hawker were in a position to deliver a modified version of their single-engined designs quickly enough. Westland, which had less work and was further advanced in their project, was chosen along with the P.88 and the Type 313 for construction. A contract for two P.9s was placed in February 1937 which were expected to be flying in mid-1938. The P.88s were ordered in December along with a Supermarine design to F37/35 but both were cancelled in January.[5]

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