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Design & Development
Second Westland Whirlwind prototype L6845 c. 1940
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.
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.
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.
Westland's design team, under the new leadership of Teddy Petter (who later designed the English Electric Canberra, Lightning and Folland Gnat) designed an aircraft that employed state-of-the-art technology. The magnesium monocoque fuselage was a small tube with a T-tail at the end, although as originally conceived, the design featured a twin tail which was discarded when large Fowler flaps were added that caused large areas of turbulence over the tail unit. The horizontal stabilizer (tailplane) was moved up out of the way of the disturbed air flow caused when the flaps were down. The engines were the Kestrel K.26, later renamed Peregrine, with internal exhaust and leading edge radiators to reduce drag. The airframe was built completely of stressed-skin duraluminium, with the pilot sitting high under one of the world's first full bubble canopies, while the low and forward location of the wing made for superb visibility (except for directly over the nose). Four 20 mm cannon were mounted in the nose; the 600 lb/minute fire rate made it the most heavily armed fighter aircraft of its era. The clustering of the weapons also meant that there were no convergence problems as with wing-mounted guns. Hopes were so high for the design that it remained "top secret" for much of its development, although it had already been mentioned in the French press.
The first prototype (L6844) flew on 11 October 1938, construction had been delayed chiefly due to the new features and also the late delivery of the engines. It was passed to RAE Farnborough at the end of the year. Further service trials were carried out at Martlesham Heath. It exhibited excellent handling and was very easy to fly at all speeds. The only exception was the inadequate directional control during takeoff which necessitated an increased rudder area above the tailplane. Production orders were contingent on the success of the test program; delays caused by over 250 modifications to the two prototypes led to an initial production order for 200 aircraft being held up until January 1939 followed by a second order for a similar number, deliveries to fighter squadrons being scheduled to begin in September 1940. Earlier, due to the lower expected production at Westland, there had been suggestions that production should be by other firms and an early 1939 plan to build them at the Castle Bromwich factory was dropped in favour of Spitfire production.
The Whirlwind was quite small, only slightly larger than the Hurricane in overall size, but smaller in terms of frontal area. The landing gear was fully retractable and the entire aircraft was very "clean" with few openings or protuberances. Radiators were in the leading edge on the inner wings rather than below the engines. This careful attention to streamlining and two 885 hp Peregrine engines powered it to over 360 mph (580 kph), the same speed as the latest single-engine fighters.
Chief test pilot of Westland, Harald Penrose flying one of the last production Whirlwinds P7110.
By late 1940, the Supermarine Spitfire was to mount 20 mm cannon, so the "cannon-armed" requirement was also being met, and by this time the role of escort fighter was becoming less important as RAF Bomber Command turned to night bomber missions. The main qualities the RAF were looking for in a twin-engine fighter were range and carrying capacity (to allow the large radar apparatus of the time to be carried), in which requirements the Bristol Beaufighter could perform just as well as or even better than the Whirlwind.
Whirlwind Mk. I/P6997 while undergoing fighter-bomber trials
at the Aeroplane and Armament Experimental Establishment.
Sources:
Gunston, Bill - The Encyclodepia of the Worlds Combat aircraft, 1976, Chartwell Books, Inc., New York
Green, William - War Planes Of The Second World War - Fighters - Vol. 2, 1961, Hanover House, New York
Wikipedia
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