Westland Whirlwind (fighter)

Last updated

Whirlwind
Westland whirlwind.jpg
Westland Whirlwind in a rare Second World War colour photograph
General information
Type Fighter aircraft
National originUnited Kingdom
Manufacturer Westland Aircraft
Primary user Royal Air Force
Number built114
History
Manufactured1940 – January 1942
Introduction dateJune 1940
First flight11 October 1938
RetiredDecember 1943

The Westland Whirlwind was a British twin-engined fighter developed by Westland Aircraft. A contemporary of the Supermarine Spitfire and Hawker Hurricane, it was the first single-seat, twin-engined, cannon-armed fighter of the Royal Air Force.

Contents

When it first flew in 1938, the Whirlwind was one of the fastest combat aircraft in the world and, with four 20 mm Hispano-Suiza HS.404 autocannon in its nose, the most heavily armed. [1] [2] Protracted development problems with its Rolls-Royce Peregrine engines delayed the project and only 114 Whirlwinds were built. During the Second World War, only three RAF squadrons were equipped with the aircraft and, despite its success as a fighter and ground attack aircraft, it was withdrawn from service in 1943.

Design and development

Westland Whirlwind second prototype, L6845, photographed at Martlesham Heath while being tested by the A&AEE, July 1939. Note the overall aluminium paint scheme, with polished spinners. Westland Whirlwind prototype.jpg
Westland Whirlwind second prototype, L6845, photographed at Martlesham Heath while being tested by the A&AEE, July 1939. Note the overall aluminium paint scheme, with polished spinners.

By the mid-1930s, aircraft designers around the world perceived that increased attack speeds were imposing shorter firing times on fighter pilots. This implied less ammunition hitting the target and ensuring destruction. 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. [4] The eight machine guns installed in the Hurricane fired rifle-calibre rounds, which did not deliver enough damage to quickly knock out an opponent, and were dispersed at ranges other than that at which they were harmonised. Cannon, such as the French 20 mm Hispano-Suiza HS.404, which could fire explosive ammunition, offered more firepower and attention turned to aircraft designs which could carry four cannon. While the most agile fighter aircraft were generally small and light, their meagre fuel capacity 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 favoured for long-range, offensive roles.

The first British specification for a high-performance machine-gun monoplane was Air Ministry specification F.5/34 for a radial-engined fighter for use in the tropics which led to four aircraft designs [lower-alpha 1] but the aircraft produced were overtaken by the development of the new Hawker and Supermarine fighters. [5] The RAF Air Staff thought that an experimental aircraft armed with the 20 mm cannon was needed urgently and specification F.37/35 was issued to British aircraft companies 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 (4,600 m). [6] [7]

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 differing in engine: Bristol Hercules radial or Rolls-Royce Vulture in-line respectively), Bristol the single-engined Type 153 with cannon in wings and the twin-engined Type 153A with cannon in nose. Hawker offered a variant of the Hurricane, the Supermarine Type 312 was a variant of the company's Spitfire [lower-alpha 2] and the Supermarine Type 313 a twin-engined (Rolls-Royce Goshawk or Hispano 12Y) design with four guns in the nose and potentially a further two firing through the propeller hubs if the 12T was used, the Westland P.9 had two Rolls-Royce Kestrel K.26 engines and a twin tail. [8] [9]

When the designs were considered in May 1936, there was concern that on the one hand a two engine design would be less manoeuvrable than a single-engined design and on the other 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. [10] Although Supermarine's efforts were favoured due to their 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 - over two years for Supermarine. [10] 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. [10]

The Westland design team, under the new leadership of W. E. W. "Teddy" Petter [lower-alpha 3] designed an aircraft that employed state-of-the-art technology. The monocoque fuselage was tubular, 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. [11] By the employment of the T-tail, the elevator was moved up out of the way of the disturbed airflow caused when the flaps were down. [11] Handley Page slats were fitted to the outer wings and to the leading edge of the radiator openings; these were interconnected by duraluminium torque tubes. [12] In June 1941, the slats were wired shut on the recommendation of the Chief Investigator of the Accident Investigation Branch, after two Whirlwinds crashed when the outer slats failed during vigorous manoeuvres; tests by the Aeroplane and Armament Experimental Establishment (A&AEE) confirmed that the Whirlwind's take-off and landing was largely unaffected with the slats locked shut, while the flight characteristics improved under the conditions in which the slats normally deployed. [13]

The engines were developments of the Rolls-Royce Kestrel K.26, later renamed Peregrine. The first prototype, L6844, used long exhaust ducts that were channelled through the wings and fuel tanks, exiting at the wing's trailing edge. This configuration was quickly changed to more conventional, external exhausts after Westland's chief test pilot Harald Penrose nearly lost control when an exhaust duct broke and heat-fractured an aileron control rod. [14] The engines were cooled by ducted radiators, which were set into the leading edges of the wing centre-sections to reduce drag. [15] The airframe was built mainly of stressed-skin duralumin, with the exception of the rear-fuselage, which used a magnesium alloy stressed skin. [16] [15] With the pilot sitting high under one of the world's first full bubble canopies and the low and forward location of the wing, all round visibility was good (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. [17] 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.

L6844 first flew on 11 October 1938, construction having been delayed chiefly due to the new features and also because of the late delivery of the engines and undercarriage. [15] L6844 was passed to RAE Farnborough at the end of the year, while further service trials were later carried out at Martlesham Heath. [18] The Whirlwind exhibited excellent handling characteristics and proved to be very easy to fly at all speeds. The only exception was the inadequate directional control during take-off which necessitated an increased rudder area above the tailplane. [11]

Whirlwind I undergoing fighter-bomber trials at the A&AEE. Whirlwind Mk I in flight, loaded w 2 500-lb GP bombs underwing, AAEE Boscombe Down.jpg
Whirlwind I undergoing fighter-bomber trials at the A&AEE.

The Whirlwind was quite small, only slightly larger than the Hurricane but with a smaller frontal area. The landing gear was fully retractable and the entire aircraft had a very clean finish with few openings or protuberances. Radiators were in the leading edge on the inner wings rather than below the engines, which contributed to the overheating problems. [19] This careful attention to streamlining and two 885 hp (660 kW) Peregrine engines powered it to over 360 mph (580 km/h), the same speed as the latest single-engine fighters. [11] The aircraft had short range, under 300 mi (480 km) combat radius, which made it as marginal as an escort as the Hurricane and Spitfire. The first deliveries of Peregrine engines did not reach Westland until January 1940.

By late 1940, the Spitfire was scheduled to mount 20 mm (0.79 in) cannon so the "cannon-armed" requirement was being met and by this time, the role of escort fighters was becoming less important as RAF Bomber Command turned to night flying. 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.

Production orders were contingent on the success of the test programme; although ACAS was impressed by the design the highly experimental design needed careful examination. [15] 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. [20] Earlier, due to the lower expected production at Westland, there had been suggestions that production should be by other firms (Fairey or Hawker) and an early 1939 plan to build 800 of them at the Castle Bromwich shadow factory was dropped in favour of Spitfire production; instead a further 200 would be built by Westland. [15] [21]

Despite the Whirlwind's promise, production ended in January 1942, after the completion of just 112 production aircraft (plus the two prototypes). Rolls-Royce needed to concentrate on the development and production of the Merlin engine, and the troubled Vulture engines, rather than the Peregrine. [22] Westland was aware that its design – which had been built around the Peregrine – was incapable of using anything larger without an extensive redesign. [23] After the cancellation of the Whirlwind, Petter campaigned for the development of a Whirlwind Mk II, which was to have been powered by an improved 1,010 hp (750 kW) Peregrine, with a better, higher-altitude supercharger, also using 100 octane fuel, with an increased boost rating. [lower-alpha 4] This proposal was aborted when Rolls-Royce cancelled work on the Peregrine. [26] [lower-alpha 5] Building a Whirlwind consumed three times as much alloy as a Spitfire. [25]

Operational history

Whirlwind Mark I, P7116 HE-F Bellows Argentina No. 2, flown by the Officer Commanding 263 Squadron RAF based at Colerne, Wiltshire, on the snow-covered airfield at Charmy Down, Somerset. Whirlwind 263 Squadron Winter 1941-1942.jpg
Whirlwind Mark I, P7116 HE-FBellows Argentina No. 2, flown by the Officer Commanding 263 Squadron RAF based at Colerne, Wiltshire, on the snow-covered airfield at Charmy Down, Somerset.

Many pilots who flew the Whirlwind praised its performance. Sergeant G. L. Buckwell of 263 Squadron, who was shot down in a Whirlwind over Cherbourg, later commented that the Whirlwind was "great to fly – we were a privileged few... In retrospect the lesson of the Whirlwind is clear... A radical aircraft requires either prolonged development or widespread service to exploit its concept and eliminate its weaknesses. Too often in World War II, such aircraft suffered accelerated development or limited service, with the result that teething difficulties came to be regarded as permanent limitations". [28] Another 263 Squadron pilot said "It was regarded with absolute confidence and affection". [29] In contrast, the test pilot Eric Brown described the aircraft as "under-powered" and "a great disappointment". [30]

An aspect of the type often criticised was the high landing speed imposed by the wing design.[ citation needed ] Because of the low production level, based on the number of Peregrines available, no redesign of the wing was contemplated, although Westland did test the effectiveness of leading-edge slats to reduce speeds. When the slats were activated with such force that they were ripped off the wings, the slats were wired shut. [31]

As the performance of the Peregrine engines fell off at altitude, perhaps a function of the propeller profile and the constant speed prop controller, [32] the Whirlwind was most often used in ground-attack missions over France, attacking German airfields, marshalling yards, and railway traffic. The Whirlwind was used to particularly good effect as a gun platform for destroying locomotives. Some pilots were credited with several trains damaged or destroyed in a mission. The aircraft was also successful in hunting and destroying German E-boats which operated in the English Channel. At lower altitudes, it could hold its own against the Messerschmitt Bf 109. Though the Peregrine was a much-maligned engine, it was more reliable than the troubled Napier Sabre engine used in the Hawker Typhoon, the Whirlwind's successor.[ citation needed ] The twin engines meant that seriously damaged aircraft were able to return with one engine knocked out. [33] The placement of the wings and engines ahead of the cockpit allowed the aircraft to absorb a great deal of damage, while the cockpit area remained largely intact. The rugged frame of the Whirlwind gave pilots greater protection than contemporary aircraft during crash landings and ground accidents.[ citation needed ] According to P. J. R. Moyes

The basic feature of the Whirlwind was its concentration of firepower: its four closely-grouped heavy cannon in the nose had a rate of fire of 600 lb./minute – which, until the introduction of the Beaufighter, placed it ahead of any fighter in the world. Hand in hand with this dense firepower went a first-rate speed and climb performance, excellent manoeuvrability, and a fighting view hitherto unsurpassed. The Whirlwind was, in its day, faster than the Spitfire down low and, with lighter lateral control, was considered to be one of the nicest "twins" ever built… From the flying viewpoint, the Whirlwind was considered magnificent. [2]

The first Whirlwinds went to 25 Squadron based at North Weald. The squadron was fully equipped with radar-equipped Bristol Blenheim IF night fighters when Squadron Leader K. A. K. MacEwen flew prototype Whirlwind L6845 from RAF Boscombe Down to RAF North Weald on 30 May 1940. [34] The following day it was flown and inspected by four of the squadron's pilots and the next day was inspected by the Secretary of State for Air, Sir Archibald Sinclair and Lord Trenchard.[ citation needed ] The first two production Whirlwinds were delivered in June to 25 Squadron for night-flying trials. [35] [36] It was then decided to re-equip 25 Squadron with the two-seat Bristol Beaufighter night fighter, as it was already an operational night fighter squadron. [37]

The first Whirlwind squadron would be 263 Squadron, which was reforming at RAF Grangemouth, after disastrous losses in the Norwegian Campaign. The first production Whirlwind was delivered to 263 Squadron by its commander, Squadron Leader H. Eeles on 6 July. [38] Deliveries were slow, with only five on strength with 263 Squadron on 17 August 1940 and none serviceable. [39] (The squadron supplemented its strength with Hawker Hurricanes to allow the squadron's pilots to fly in the meantime.) [37] Despite the Battle of Britain and the consequent urgent need for fighters, 263 Squadron remained in Scotland, Air Chief Marshal Hugh Dowding, in charge of RAF Fighter Command, stated on 17 October that 263 could not be deployed to the south because "there was no room for 'passengers' in that part of the world". [36]

Whirlwind showing the new "Type B" paint scheme introduced in November 1940: while the black underside to the port wing was temporary, the sky fuselage band was a longer-lasting change. Westland Whirlwind 263 Sqn Exeter, banking awf cam, fighter paint 1940nov27-crop.jpg
Whirlwind showing the new "Type B" paint scheme introduced in November 1940: while the black underside to the port wing was temporary, the sky fuselage band was a longer-lasting change.

The first Whirlwind was written off on 7 August when Pilot Officer McDermott had a tyre blow out while taking off in P6966. In spite of this he managed to get the aircraft airborne. Flying Control advised him of the dangerous condition of his undercarriage. PO McDermott bailed out of the aircraft between Grangemouth and Stirling. The aircraft dived in and buried itself eight feet into the ground. [40] On recent inspection of the salvaged wreck of P6966, it was noticed that the defective tyre fitted was not of the correct size for a Whirlwind. Instead, it was the correct size for a Hurricane which 263 Squadron was also flying.

No. 263 Squadron moved south to RAF Exeter and was declared operational with the Whirlwind on 7 December 1940. [38] Initial operations consisted of convoy patrols and anti E-boat missions. [38] [41] The Whirlwind's first confirmed kill occurred on 8 February 1941, when an Arado Ar 196 floatplane was shot down; the Whirlwind responsible also crashed into the sea and the pilot was killed. [42] From then on the squadron was to have considerable success with the Whirlwind while flying against enemy Junkers Ju 88, Dornier Do 217, Messerschmitt Bf 109s and Focke-Wulf Fw 190s.

263 Squadron also occasionally carried out day bomber escort missions with the Whirlwinds. One example was when they formed part of the escort of 54 Blenheims on a low-level raid against power stations near Cologne on 12 August 1941; owing to the relatively short range of the escorts, including the Whirlwinds, the fighters turned back near Antwerp, with the bombers continuing on without escort. Ten Blenheims were lost. [43] [44]

The squadron mostly flew low-level attack sorties across the channel ("Rhubarbs" against ground targets and "Roadstead" attacks against shipping). [42] The Whirlwind proved a match for German fighters at low level, as demonstrated on 6 August 1941, when four Whirlwinds on an anti-shipping strike were intercepted by a large formation of Messerschmitt Bf 109s and claimed three Bf 109s destroyed for no losses. [43] A second Whirlwind squadron, 137, formed in September 1941, specialising in attacks against railway targets. [42] [45] In the summer of 1942, both squadrons were fitted with racks to carry two 250 or 500 lb (110 or 230 kg) bombs, and nicknamed 'Whirlibombers'. [46] [47] These undertook low-level cross-channel "Rhubarb" sweeps, attacking locomotives, bridges, shipping and other targets.

Three Westland Whirlwinds of 263 Squadron in stepped line-astern formation 3 Westland Whirlwinds of 263 Sqn Exeter(Devon), flying in stepped line-astern formation over West Country.jpg
Three Westland Whirlwinds of 263 Squadron in stepped line-astern formation

The worst losses of 137 Squadron occurred on 12 February 1942 when they were sent to escort five British destroyers, unaware of the escaping German warships Scharnhorst and Gneisenau making the Channel Dash to safer ports. Four Whirlwinds took off at 13:10 hours and soon sighted warships through the clouds about 20 mi (32 km) from the Belgian coast. They descended to investigate and were immediately jumped by about 20 Bf 109 fighters of Jagdgeschwader 2. The Whirlwinds shot at anything in their sights but were heavily outnumbered. While this was happening, at 13:40, two more Whirlwinds were sent up to relieve the first four and two more Whirlwinds took off at 14:25; four of the eight Whirlwinds failed to return.

From 24 October until 26 November 1943, Whirlwinds of 263 Squadron made several heavy attacks against the German blockade runner Münsterland , in dry dock at Cherbourg. As many as 12 Whirlwinds participated at a time in dive bombing attacks carried out from 12,000–5,000 ft (3,700–1,500 m) using 250 lb (110 kg) bombs. The attacks were met by very heavy anti-aircraft fire but virtually all bombs fell within 500 yd (460 m) of the target; only one Whirlwind was lost during the attacks.

The last Whirlwind mission to be flown by 137 Squadron was on 21 June 1943, when five Whirlwinds took off on a "Rhubarb" attack against the German airfield at Poix. [45] P6993 was unable to locate the target and instead bombed a supply train north of Rue. While returning, the starboard throttle jammed in the fully open position and the engine eventually lost power. It made a forced landing in a field next to RAF Manston but the aircraft was a write-off, although, as in many other crash landings in the type, the pilot walked away unhurt.

No. 263 Squadron, the first and last squadron to operate the Whirlwind, flew its last Whirlwind mission on 29 November 1943, turning in their aeroplanes and converting to the Hawker Typhoon in December that year. [48] On 1 January 1944, the type was declared obsolete. [49] The remaining serviceable aircraft were transferred to No. 18 Maintenance Unit, while those undergoing repairs or overhaul were allowed to be repaired only if they were in near-flyable condition. An official letter forbade aircraft needing repair to be worked on.

P6969 'HE-V' of 263 in flight over the West Country Whirlwind Mk I, 263 Sqn Exeter, in flight over West Country.jpg
P6969 'HE-V' of 263 in flight over the West Country

The aircraft was summed up by Francis Mason as follows:

Bearing in mind the relatively small number of Whirlwinds that reached the RAF, the type remained in combat service, virtually unmodified, for a remarkably long time…The Whirlwind, once mastered, certainly shouldered extensive responsibilities and the two squadrons were called upon to attack enemy targets from one end of the Channel to the other, by day and night, moving from airfield to airfield within southern England. [50]

Variants

P.9 prototype

Single-seat twin-engine fighter aircraft prototype. Two built (L6844 and L6845), can be distinguished from later production samples by the mudguards above the wheels (as did the first production sample, P6966), the exhaust system and the so-called 'acorn' on the joint between fin and rudder. L6844 had a distinctive downward kink to the front of its pitot tube, atop the tail not seen again in following models. L6844's colour was dark grey. L6844 had opposite-rotation engines, L6845 had engines that rotated in the same direction; this carried over to production machines.

Whirlwind I

Single-seat twin-engine fighter aircraft, 400 ordered, 116 built (2 prototypes and 114 production versions).

Whirlwind II

Single-seat twin-engine fighter-bomber aircraft, fitted with underwing bomb racks, were nicknamed "Whirlibombers". At least 67 conversions made from the original Mk I fighter.

Experimental variants A Mk I Whirlwind was tested as a night fighter in 1940 with No. 25 Squadron. The first prototype was armed with an experimental twelve 0.303 (7.7 mm) machine guns and another one 37 mm cannon. [29] [51]

Merlin variant Westland proposed fitting Merlin engines in a letter to Air Marshal Sholto Douglas. [52] The proposal was rejected but Westland used the design work already performed in developing the Welkin high-altitude fighter.

Operators

Flag of the United Kingdom.svg  United Kingdom

US Navy One aircraft P6994 was sent to the US for trials in June 1942 and survived there until at least late 1944.

Survivors

After retirement in December 1943, all but one of the surviving Whirlwinds were sent to No. 18 Maintenance Unit RAF at Dumfries, Scotland, where they were scrapped. P7048 was retained by Westland and was granted a civil certificate of airworthiness on 10 October 1946, with the registration G-AGOI. It was used as a company hack for a short time before being withdrawn in 1947 and scrapped. [49] [53] In October 1979, the remains of Whirlwind P6966, the first Whirlwind to be lost, were recovered near Grangemouth by enthusiasts in a dig group. The two Peregrine engines were recovered, as well as many pieces of the airframe. [40] The Whirlwind Fighter Project began building a full-scale replica Whirlwind in 2011–2012. By 2023 an authentic cockpit section had been built and put on display at the Kent Battle of Britain Museum in Hawkinge. [54] Plans for a 2/3 scale replica were marketed for home building in the late 1970s and early 1980s as the Butterworth Westland Whirlwind. [55]

Specifications (Whirlwind I)

Chief test pilot of Westland, Harald Penrose flying one of the last production Whirlwinds P7110. Whirlwindfighterproject FA 18181s.jpg
Chief test pilot of Westland, Harald Penrose flying one of the last production Whirlwinds P7110.

Data from Westland's Double Trouble [56]

General characteristics

Performance

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

Related Research Articles

<span class="mw-page-title-main">Westland Welkin</span> British twin-engine heavy fighter

The Westland Welkin was a British twin-engine heavy fighter from the Westland Aircraft Company, designed to fight at extremely high altitudes, in the stratosphere; the word welkin meaning "the vault of heaven" or the upper atmosphere. First conceived in 1940, the plane was built in response to the arrival of modified Junkers Ju 86P bombers flying reconnaissance missions, which suggested the Luftwaffe might attempt to re-open the bombing of England from high altitude. Construction was from 1942 to 1943. The threat never materialised; consequently, Westland produced only a small number of Welkins and few of these flew.

<span class="mw-page-title-main">Hawker Tempest</span> British fighter aircraft

The Hawker Tempest is a British fighter aircraft that was primarily used by the Royal Air Force (RAF) in the Second World War. The Tempest, originally known as the Typhoon II, was an improved derivative of the Hawker Typhoon, intended to address the Typhoon's unexpected deterioration in performance at high altitude by replacing its wing with a thinner laminar flow design. Since it had diverged considerably from the Typhoon, it was renamed Tempest. The Tempest emerged as one of the most powerful fighters of World War II and at low altitude was the fastest single-engine propeller-driven aircraft of the war.

<span class="mw-page-title-main">Supermarine Seafire</span> Carrier-based fighter aircraft

The Supermarine Seafire is a naval version of the Supermarine Spitfire fighter adapted for operation from aircraft carriers. It was analogous in concept to the Hawker Sea Hurricane, a navalised version of the Spitfire's stablemate, the Hawker Hurricane. The name Seafire was derived from the contraction of the full name of Sea Spitfire.

<span class="mw-page-title-main">Supermarine Attacker</span> Carrier-based fighter aircraft; first jet fighter in Royal Navy service

The Supermarine Attacker is a British single-seat naval jet fighter designed and produced by aircraft manufacturer Supermarine for the Royal Navy's Fleet Air Arm (FAA). It was the first jet fighter to enter operational service with the FAA.

<span class="mw-page-title-main">Supermarine Swift</span> British single-seat jet-propelled fighter aircraft

The Supermarine Swift is a British single-seat jet fighter aircraft that was operated by the Royal Air Force (RAF). It was developed and manufactured by Supermarine during the 1940s and 1950s. The Swift featured many of the new jet age innovations, such as a swept wing. On 26 September 1953, a Swift F.4 piloted by Commander Mike Lithgow broke the world absolute speed record, reaching a speed of 737.7 mph (1,187 km/h).

<span class="mw-page-title-main">Supermarine Spitfire (late Merlin-powered variants)</span> Late Merlin-powered variants of the Supermarine Spitfire

The British Supermarine Spitfire was facing several challenges by mid-1942. The debut of the formidable Focke-Wulf Fw 190 in late 1941 had caused problems for RAF fighter squadrons flying the latest Spitfire Mk Vb. Rolls-Royce engineers were already working on a new version of the Merlin incorporating a two-stage supercharger; the combination of the improved Merlin and the Spitfire Mk Vc airframe in a "stop-gap" design allowed the RAF to combat the Fw 190 on equal terms.

<span class="mw-page-title-main">W. E. W. Petter</span> British aircraft designer (1908 – 1968)

William Edward Willoughby "Teddy" Petter was a British aircraft designer. He is noted for Westland's wartime aeroplanes, as well as the Canberra, the early design of the Lightning, and his last plane, the Folland Gnat.

<span class="mw-page-title-main">Supermarine Spiteful</span> 1944 British fighter aircraft

The Supermarine Spiteful was a British fighter aircraft designed by Supermarine during the Second World War as a successor to the Spitfire. Powered by a Rolls-Royce Griffon engine, it had a radical new wing design to allow safe operations at higher speeds and incorporating inwards-retracting undercarriage. Other changes included a larger fin to improve the marginal stability of Griffon Spitfires. Development of the wing was formalised by Air Ministry specification F.1/43; as well as a new aircraft, there was an expectation the wing could be used as a replacement for the elliptical wing on Spitfire production.

<span class="mw-page-title-main">Rolls-Royce Peregrine</span> 1930s British aircraft piston engine

The Rolls-Royce Peregrine was a 21-litre (1,300 cu in), 885-horsepower (660 kW) liquid-cooled V-12 aero engine designed and built by the British manufacturer Rolls-Royce in the late 1930s. It was essentially the ultimate development of the company's Kestrel engine, which had seen widespread use in military aircraft of the pre-war period.

<span class="mw-page-title-main">Supermarine Seafang</span> 1940s British fighter aircraft

The Supermarine Seafang was a British Rolls-Royce Griffon–engined fighter aircraft designed by Supermarine to Air Ministry specification N.5/45 for naval use. It was based on the Spiteful, which was a development of Supermarine's Griffon-engined Spitfire aircraft. By that time the Spitfire was a 10-year-old design in a period of rapid technical development in aviation. The Seafang was outmoded by jet aircraft, and only 18 were built.

<span class="mw-page-title-main">No. 263 Squadron RAF</span> Former flying squadron of the Royal Air Force

No 263 Squadron was a Royal Air Force fighter squadron formed in Italy towards the end of the First World War. After being disbanded in 1919 it was reformed in 1939 flying mainly strike and heavy fighter aircraft until becoming No 1 Squadron in 1958.

<span class="mw-page-title-main">RAF Fairwood Common</span> Former Royal Air Force station in Swansea, Wales

Royal Air Force Fairwood Common, or more simply RAF Fairwood Common, is a former Royal Air Force Sector Station located on Fairwood Common, on the Gower Peninsula, to the west of Swansea. It is now the location of Swansea Airport.

<span class="mw-page-title-main">Supermarine Type 224</span> British prototype fighter

The Supermarine Type 224 was a British gull-wing monoplane fighter aircraft designed by R.J. Mitchell at Supermarine in response to Air Ministry Specification F.7/30, which sought to introduce a new fighter to succeed the Gloster Gauntlet. The Type 224 was powered by a Rolls-Royce Goshawk engine, which used an experimental evaporative cooling system.

No. 225 Squadron RAF is a former Royal Air Force squadron.

<span class="mw-page-title-main">Supermarine Spitfire (early Merlin-powered variants)</span> Early variants of the Supermarine Spitfire

Supermarine Spitfire variants powered by early model Rolls-Royce Merlin engines mostly utilised single-speed, single-stage superchargers. The British Supermarine Spitfire was the only Allied fighter aircraft of the Second World War to fight in front line service from the beginnings of the conflict, in September 1939, through to the end in August 1945. Post-war, the Spitfire's service career continued into the 1950s. The basic airframe proved to be extremely adaptable, capable of taking far more powerful engines and far greater loads than its original role as a short-range interceptor had called for. This would lead to 19 marks of Spitfire and 52 sub-variants being produced throughout the Second World War, and beyond. The many changes were made in order to fulfil Royal Air Force requirements and to successfully engage in combat with ever-improving enemy aircraft. With the death of the original designer, Reginald J. Mitchell, in June 1937, all variants of the Spitfire were designed by his successor, Joseph Smith, and a team of engineers and draftsmen.

<span class="mw-page-title-main">RAF Matlaske</span> Former RAF station in Norfolk, England

Royal Air Force Matlaske or more simply RAF Matlaske is a former Royal Air Force satellite station to RAF Coltishall, situated near Matlaske in Norfolk, England.

<span class="mw-page-title-main">RAF Angle</span> Former Royal Air Force station in Pembrokeshire, Wales

Royal Air Force Angle or more commonly RAF Angle, is a former Royal Air Force station located on the Angle Peninsula Coast, 8 miles (13 km) west of Pembroke, Pembrokeshire, Wales. It was operational from 1 June 1941 to 11 July 1946, having been used by both the Royal Air Force and the Royal Navy.

<span class="mw-page-title-main">Supermarine Spitfire (Griffon-powered variants)</span> Griffon-powered variants of the Supermarine Spitfire

The Rolls-Royce Griffon engine was designed in answer to Royal Navy specifications for an engine capable of generating good power at low altitudes. Concepts for adapting the Spitfire to take the new engine had begun as far back as October 1939; Joseph Smith felt that "The good big 'un will eventually beat the good little 'un." and Ernest Hives of Rolls-Royce thought that the Griffon would be "a second power string for the Spitfire". The first of the Griffon-engined Spitfires flew on 27 November 1941.

<span class="mw-page-title-main">Supermarine Spitfire</span> British single-seat WWII fighter aircraft

The Supermarine Spitfire is a British single-seat fighter aircraft used by the Royal Air Force and other Allied countries before, during, and after World War II. It was the only British fighter produced continuously throughout the war. The Spitfire remains popular among enthusiasts. Around 70 remain airworthy, and many more are static exhibits in aviation museums throughout the world.

The Supermarine Type 324 and Type 325 were British two-engined fighter designs proposed as the replacement for the Supermarine Spitfire and Hawker Hurricane. Neither of them nor a revised design - the Type 327 - to carry cannon was accepted for development and production.

References

Notes

    1. these were the Gloster F.5/34, Martin-Baker MB 2, Bristol Type 146, and Vickers Venom
    2. The Spitfire was then in development for F.37/34 and Supermarine suggested that a second set of wings would mean one aircraft design could meet both specifications
    3. Petter left Westland in 1944 and later designed the English Electric Canberra, English Electric Lightning and Folland Gnat
    4. Using 100 octane fuel, the standard Peregrine could use up to +9 lb/sq in (62 kPa) boost for take-off or operations. [24] The improved Peregrine envisaged by Petter would use +12 lb/sq in (83 kPa) and be rated to 20,000 ft (6,100 m). [25]
    5. Additional proposals included the use of Bristol-built or American radial engines, while another possibility mooted in 1941 was to use two 1,400 hp (1,000 kW) Merlin XX engines. [27] [25]

    Citations

    1. Rickard, J (21 November 2007). "Westland Whirlwind". historyofwar.org.
    2. 1 2 Moyes 1967, pp. 278–279.
    3. Franks 2014, pp. 44–45, 56.
    4. Buttler 2004, p.7
    5. Buttler 2004, p.8
    6. Bingham 1987, pp. 14–15.
    7. Meekoms & Morgan 1994, pp. 217–218.
    8. Bingham 1987, pp. 14–16.
    9. Buttler 2004, pp. 34–35
    10. 1 2 3 Buttler 2004, pp. 36–37
    11. 1 2 3 4 Green 1964, p. 51.
    12. Bingham 1987, p. 55.
    13. Corduroy 2013, p. 68.
    14. Bingham 1987, p. 28.
    15. 1 2 3 4 5 Buttler 2004, p. 37.
    16. Bingham 1987, p. 57.
    17. Moyes 1967, p.3.
    18. Moyes 1967, p. 5.
    19. "The Westland Whirlwind British fighter aircraft of WW2". Dingeraviation.net. Retrieved 2 May 2022.
    20. James 1991, p. 263.
    21. Corduroy 2013, p. 33.
    22. Corduroy 2013, pp. 35–36.
    23. Buttler 2004, p. 38.
    24. Air Ministry 1940, Vol 1, Sect 2 Para 29.
    25. 1 2 3 Corduroy 2013, p. 44.
    26. Corduroy 2013, pp. 40–42
    27. Bingham 1987, pp. 40, 42.
    28. Mason 1969
    29. 1 2 Robertson 1970, p. 16.
    30. Captain Eric 'Winkle' Brown - test pilot legend (Part2), Royal Aeronautical Society, 27 September 2010, archived from the original on 30 March 2013 via Youtube
    31. James 2006, p. 65.
    32. Bearman, Matt (2 August 2023). "It Wasn't the Engine That Did in the Westland Whirlwind — What Was It?". HistoryNet. Retrieved 24 August 2023.
    33. Bingham 1987, p. 45
    34. James 1991, p. 268.
    35. James 1991, pp. 268–269.
    36. 1 2 Buttler 2002, p. 11.
    37. 1 2 James 1991, p. 269.
    38. 1 2 3 Heffernan 1985, p. 62.
    39. Price 1995, p. 162.
    40. 1 2 "RAF Westland Whirlwind / P6966.", Air Crash Sites Scotland, 2011, archived from the original on 26 October 2018, retrieved 20 September 2013
    41. James 2006, pp. 70–71.
    42. 1 2 3 James 2006, p. 71.
    43. 1 2 3 Price 1995, p. 163.
    44. Richards 1995, pp. 118–119.
    45. 1 2 Buttler 2002, p. 15.
    46. Buttler 2002, pp. 14–15.
    47. James 1991, p. 270.
    48. James 2006, pp. 71–72.
    49. 1 2 James 2006, p. 73.
    50. Mason 1969, p. 64.
    51. Green 1961, p. 125.
    52. PRO/NA air 16-326 page 82A
    53. Buttler 2002, p. 16.
    54. "whirlwind". WFP. Retrieved 23 July 2023.
    55. Taylor 1982, p. 534.
    56. James 2006, p. 69.
    57. James 1991, pp. 370–371.

    Bibliography

    Further reading