Westland Whirlwind (fighter) - Design and Development

Design and Development

The British Air Ministry, issued specification F.37/35 in 1935, calling for a single-seat day and night fighter armed with four cannon. Six aircraft were submitted in response to the specification, of which three were twin-engined types: the Boulton Paul P.88, the Bristol Type 153A, the Hawker F.37/35 (which was a Hurricane variant), the Supermarine 312 (a Spitfire variant), the Supermarine 313 and the Westland P.9.

Although Supermarine's efforts were favoured due to their success previously 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 aircraft quickly enough. Westland which had less work and was more advanced in the 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, making 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. Further Service Trials 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 km/h), the same speed as the latest single-engine fighters.

But there were problems as well. The aircraft had limited range, under 300 miles combat radius, which made it marginal as an escort. More troublesome were the continued failures of the Peregrine engine. It was originally intended to be one of Rolls' main designs, but the Merlin had become much more important to the war effort and the Peregrine was relegated to a secondary status and development cancelled (there being no other aircraft needing the engine); the first deliveries of Peregrine engines did not reach Westland until January 1940.

By 1940, the Supermarine Spitfire was mounting 20 mm cannons, 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.

Development and delivery problems with the Peregrine engines, along with a number of flying accidents and the aircraft’s high landing speed (which restricted the number of airfields from which it could operate), resulted in Whirlwind production being ended in January 1942, after the completion of just 112 production aircraft. Westland campaigned for the creation of a Mk II model, initially designed around a more powerful 1,010 hp Peregrine which was aborted owing to Rolls-Royce's cancellation of further development of the engine. Additional proposals by Petter similarly remained as "paper projects" and included re-engining with Bristol Hercules, American radials and even using two 1,400 hp Merlin XX engines, each concept being rejected by the Air Ministry. Westland were aware that their design - which had been built around the Peregrine was incapable of being re-engined with anything larger.