US Pacific fighters versus the Luftwaffe Bf 109 and Fw 190

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A reader of our site asked us how US Pacific fighters would fare against the Luftwaffe’s finest – the Messerschmitt Bf 109 and Focke-Wulf Fw 190. Curious to know more we asked HushKit contributor Edward Ward to consider the matter. 

The interesting thing about the F4F, F6F and F4U is that we do have a tantalising hint of their efficacy against late Luftwaffe fighters as all three were used by the Fleet Air Arm in Europe. Sadly (in a way) the Corsair never met a German fighter in combat but both the Grummans did and the results were positive. Oddly, despite never actually engaging in air-to-air combat over Europe, a Corsair was captured by the Luftwaffe and extensively tested by them. The results for the Grummans were more interesting. Surprisingly the first American-built aircraft to score a kill in British service was a Wildcat (then named a Martlet) when two Martlet Is of 804 sqn Fleet Air Arm shot down a Junkers 88 on Christmas Day 1940. Later Martlets operated in the Western Desert in a shore based role. Finding out detailed information abut this period is difficult. About the best I can manage is that they operated in “ground attack and escort missions” so one would have thought they would have met the Luftwaffe however I can only find records for one FIAT G.50 and four Ju 88s shot down. More research needed. There is an Osprey ‘Aircraft of the Aces’ volume on Royal Navy aces of WWII that would I suspect give an excellent account of this period but alas I don’t own it… All this occurred before the US had even entered the war.

This is what Eric Brown had to say about the Martlet/Wildcat and its chances against the Luftwaffe. It is worth noting that although more famous as a test pilot, Eric Brown had flown the Martlet in combat from escort carriers against Fw 200 Condors.
Martlet II Versus Messerschmitt Bf 109F

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The Wildcat, although faster and more manoeuvrable than the Sea Hurricane, was still some 60mph slower than the German fighter. The lower the altitude the less the odds favoured the Me109F. The Wildcat also had a heavier punch to deliver.

Verdict: As a dogfighter the Wildcat was superior to the Me 109F, but the initiative always lay with the German because of superior performance. At low altitudes the Me109F had the edge over the Wildcat, but not by much.

Martlet IV Versus Focke-Wulf 19A-4 and A-4/U8: The only superiority that could be claimed by the Wildcat was its ability to outturn the German fighter, but turning doesn’t win battles. In every other department the Fw 190 was in command. Even in the fighter-bomber role the German faced minimal danger, and he could always jettison his bombs in an emergency to defend himself.
Verdict: The superiority of the Fw 190A-4 and A-4/U8 was so comprehensive that the Wildcat had little or no chance to do anything more than perhaps harry the German enough to make him jettison his bombs prematurely.

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However by the time the Wildcat VI was on the scene (1944) his assessment was rather less rosy: “Wildcat VI Versus Messerschmitt 109G-6: The agile little Wildcat could outmanoeuvre the latest version of the Me 109, but the performance differential had widened and the German could run rings around the Wildcat. If the Me 109G-6 was tempted to mix it in a dogfight, the Wildcat had a better than even chance of success.Verdict: The Wildcat was no real match for the Me 109G-6, but the German could not afford to take liberties with his angry little opponent.”

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The formidable Fw 190 held all the advantages in this contest, and there was really no way out of the dilemma for the Wildcat. Even in a turning circle it could not evade the German fighter for the first 120 degrees, and that was more than enough time for the powerful armament of the Fw 190 to take effect.

Verdict: The Wildcat had little chance of surviving single combat with the Fw 190. Its only hope lay in overwhelming the German by force of numbers.

Ultimately most RN Martlets and Wildcats saw service on escort carriers, far from German fighters. However, despite its apparent performance shortfall, In March 1945, Wildcats shot down four Messerschmitt Bf 109Gs over Norway. These were the FAA’s last victories with Wildcats.

With regard to the Hellcat, only the Royal Navy actually flew it in combat against Luftwaffe fighters. US Hellcats did see service over Europe when they operated off USS Tulagi during Operation Dragoon (the invasion of Southern France) in August 1944. During Dragoon, USN Hellcats shot down eight German aircraft but all were bombers or transports. A year or so earlier, four British Hellcats were bounced by a mixture of Fw 190s and Bf 109Gs off the Norwegian coast. One Hellcat was lost but the other three each claimed the destruction of one German fighter each. Hardly much to go on but the Hellcat came out on top in that action at least.

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If I were to speculate on what would have happened had the two later Navy aircraft been deployed in numbers in Europe I suspect a similar situation as that which developed with the P-47 and P-51 would have developed, the Hellcat is slower than the Corsair (and very much slower than either a Thunderbolt or a Mustang) but is a very forgiving aircraft and also insanely rugged (a proportionately much greater number of F6Fs survived being hit by flak for example than did F4Us) and thus it would seem likely that the Hellcat would be employed more as a fighter bomber rather than a straight air-to-air fighter. If intercepted the Hellcats exceptional manoeuvrability (it could follow the A6M Zero through most manoeuvres, and that aircraft may well have been the most agile of the war) would have proved difficult to deal with for both German fighters but they would have been able to break off at will.

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The F4U was a rather different prospect, with a significantly better performance than the Hellcat it is likely that any service it might have given against the Luftwaffe would have been impressive. There are caveats however – the afore-mentioned Eric Brown said he would prefer the Hellcat in a dogfight, however during the second world war pilots in every nation (except maybe Japan) were desperately trying to avoid dogfighting wherever possible and use dive and zoom climb tactics. This would have favoured the Corsair which excelled in the vertical plane. Whether it would have done as well as it did against the Japanese is unlikely however. The Luftwaffe, although a shadow of its former self by 1945 was still a dangerous foe and did not suffer the same technological disparity (in general) as did the late war Japanese fighters compared to their principal American adversaries. It is possible of course that it may not have fared so well, the P-39 Airacobra was generally regarded as unsatisfactory in the Pacific theatre yet was extremely successful against the Germans over the Eastern Front (of US built fighters only the P-51 would score more air to air kills) However, we do have at least a glimpse of what might have transpired in reality as the US tested the Fw 190 against the F4U and F6F and the results are here. It is worth noting however that the Focke Wulf in this case was an early model and not indicative of the models that the Corsair and Hellcat would have actually met in combat had they been committed to the European theatre.

In short, what would actually have transpired is anyone’s guess. The American fighters were formidable but then, so were the German aircraft. It may have depended a great deal on when they were committed. Corsairs fist flew into combat in August 1942, at that point the Luftwaffe was still probably the most powerful, best trained, most experienced and arguably best equipped Air Force in the world. Any fighter thrown at them at that time would have suffered. Had the Luftwaffe of early 1945 been their foe though it would have been a different story as most of the veterans were either dead or wounded, there was precious little fuel for operations and the training programme had collapsed.

All of which is a long-winded way of saying it’s pretty much anyone’s guess what would have actually happened.

— Edward Ward

 

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Dornier Do 31: the jump-jet tactical transport that actually flew

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Jim Smith had significant technical roles in the development of the UK’s leading military aviation programmes. From ASRAAM and Nimrod, to the JSF and Eurofighter Typhoon. We asked his opinion on what we can learn from the Dornier Do 31. 

As with the Royal Air Force, in the early 1960s, the Luftwaffe became concerned about the vulnerability of aircraft operating from large air bases.  The British developed and eventually deployed the Harrier; the Germans, in a frenzy of innovation, developed and flew, but did not put into service, two potentially supersonic VTOL fast-jets, and a VTOL transport, the Do 31E. They also experimented with a zero-length launch system for the Starfighter, the ZELL.

The two fast-jets were the VFW VAK 191, which was intended as a strike aircraft with a limited supersonic dash capability, and the EWR VJ 101C, which was a Mach 1.8-capable VTOL interceptor. The Do 31, as a production aircraft, was envisaged as supplying tactical logistic support to the fast jets, itself using as forward operating bases the airstrips on which the ZELL Starfighters were expected to land using arrester gear.

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image005.jpgThe events at the start of the Six Day War between Israel and Egypt in 1967 showed that the concern about the vulnerability of aircraft on the ground at airbases was somewhat justified. Israel essentially destroyed the capability of the Egyptian Air Force in strikes against their airbases in the first hours of the conflict. At that time, the aircraft discussed here were all in development.

Do 31E Configuration

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The Dornier 31E3 shown in the heading photo was the first, and to date, the only jet VTOL transport aircraft to fly, doing so in the E3 version in July 1967. In December of that year, the aircraft successfully completed transition from vertical take-off to forward flight, and the reverse transition to vertical landing. To do this, it operated with no less than 10 engines, two 15,000lb thrust Pegasus engines in the mid-span nacelles, and a further 4 Rolls-Royce RB 162-4D lift engines in each wing tip pod, each providing a further 4,400lb thrust. Total thrust was an impressive 65,200lb, providing some margin for hot-gas re-ingestion and suckdown effects at the maximum take-off weight of 60,600lb (Data from Janes All the World’s Aircraft 1966-67).

Payload capability was 36 fully equipped troops, or ‘two or three’ Jeeps, or palleted freight, up to a maximum of 11,000lb, and a range of 1100 miles was expected with maximum payload.

The Problems

Given the quite impressive technical achievements of the design, you may wonder why the Do 31 appears in this list. The real problem with this aircraft, and indeed the associated EWR VJ101C and VFW VAK 191B, was with the totally unachievable operating concept. It turns out that airbases (and aircraft carriers) provide really useful capabilities supporting tactical aircraft.

Without some form of operating base, maintenance, spares, fuel, accommodation, mission preparation, and protection and shelter of aircrew and maintenance personnel become major logistic problems.

When you add to this the impact on cost and complexity, weight and drag, of carrying around 10 engines, only 2 of which are used in forward flight, it becomes clear that the Dornier 31E was really up against it, both operationally and technically.

The Eventual Solution

What was the resolution, beyond cancelling all the related projects? Well, once the difficulty of operating without airbase infrastructure had been considered, the answer was to effectively protect the airbases with capable surface-to-air defences, and to protect the aircraft and support infrastructure with appropriate hardened shelters. This enabled conventional solutions to be found to the tactical requirements of most air forces, noting, however, the extremely effective use of carrier-borne (or forward-based) Harriers in support of operations by the US Marines, RAF and a number of Navies.

The tactical and logistic support of forward air operations, it turns out, can be well supported by another aircraft which was in development at the time – the Fiat G222. This has now been developed into today’s C-27 Spartan, which offers similar payload-range performance to the Dornier 31E, albeit with STOL rather than VTOL capability, at a fraction of the cost, risk and complexity of a production Do 31.

Was it worth the effort

Was the Do-31 (and for that matter, the other related projects) worth the effort? Well, all three aircraft explored the difficult VSTOL regimes, with quite challenging requirements. There is no doubt that German Industry gained significantly in understanding computer-assisted control of some advanced and challenging designs.  This may well have helped the Industry play its part in the later development of the Tornado and Eurofighter.

That said, no operational system eventuated, mainly, I suggest, because technical progress had run ahead of operational analysis, resulting in flawed requirements.

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Jim Smith had significant  roles in the development of the UK’s leading military aviation programmes. His latest book is available here.

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Have a look at How to kill a Raptor, An Idiot’s Guide to Chinese Flankers, the 10 worst British military aircraft, The 10 worst French aircraft,  Su-35 versus Typhoon, 10 Best fighters of World War II , top WVR and BVR fighters of today, an interview with a Super Hornet pilot and a Pacifist’s Guide to Warplanes. Was the Spitfire overrated? Want something more bizarre? The Top Ten fictional aircraft is a fascinating read, as is The Strange Story and The Planet Satellite. The Fashion Versus Aircraft Camo is also a real cracker. Those interested in the Cold Way should read A pilot’s guide to flying and fighting in the Lightning. Those feeling less belligerent may enjoy A pilot’s farewell to the Airbus A340. Looking for something more humorous? Have a look at this F-35 satire and ‘Werner Herzog’s Guide to pusher bi-planes or the Ten most boring aircraft. In the mood for something more offensive? Try the NSFW 10 best looking American airplanes, or the same but for Canadians. 

Aviation beauty pageant 2019: Readers’ vote

airplane_jet_fighter_flanker_airshow_military_sukhoi_su_27-1170481We asked Hush-Kit followers to vote on the which aircraft were the most beautiful. Surprisingly, their voting choices were not completely insane. 

Round 1 

Widebody booty

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Boeing Dreamliner 787 Dreamliner

Versus

Airbus A350 XWB 

With its sharky tail, sawtooth engine nacelles and slimmer body we expected the Dreamliner to walk this, but the results were tighter than the elbows of EasyJet passengers. Both aircraft have lovely noses, with the A350 having a more distinctive cockpit windows, like a fast train wearing goggles. Wingwise the Dreamliner has the edge, with its lovely raked back tips and flappy flexibility.

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Round 2

European Middleweight clash 

Eurofighter Typhoon 

versus

Dassault Rafale 

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The Matt & Luke of the fighter world, the Typhoon and Rafale are very similar yet provoke more rows than almost any other two types. The Typhoon suffers from a plasticy look, a fussy boxy intake and a lack of curves, the Rafale a dorky 60s refuelling probe and what looks like a catering-size box of clingfilm strapped onto its fin. Clearly, this had to go to Rafale, because despite Typhoon’s noble canopy, lovely nose and decent proportions, the French aircraft is far prettier. Rafale TF-102-esque forward fuselage and kidney intakes are an absolute treat of delicious Henry Moore curves, the canards are a small and perky detail set neatly close to the not overly large wing. The overall design is compact with some lovely detail features such as the gold flash cockpit and serrated stealthy panel edges. The unusual jet nozzles are rather bland but overall the Rafale is a beautiful aircraft, something reflected in readers’ votes.

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Round 3

Fourth Gen Heavyweights 

McDonnell Douglas F-15 Eagle

Versus

Sukhoi T-10 ‘Flanker’ series 

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Bill Sweetman noted that the the ‘Flanker’ “..looks incomparably bad-ass, as if God designed a pterodactyl to go Mach 2.” and our readers generally agreed. The Eagle is beautiful too, but more butch than elegant (with its undercarriage out the F-15 does look very awkward).

 

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Round 4

Supersonic airliners 

Tupolev Tu-144

Versus

Aérospatiale/BAC Concorde

A poetic swan or Darth Vader’s weekend runaround? Come on!

 

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Almost the greatest fighter of World War II: The Martin-Baker MB5

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Photo copyright BAE Systems from the DH Propellers Archive

Imagine a world without Danny DeVito, Roger Daltrey and George Lucas. There’s a parallel universe where Rick Moranis played Schwarzenegger’s brother in Twins, where The Who never happened and where Star Wars was a military project to make Reagan hard and the Soviet Union broke. This speculative universe is one in which famous figures born in 1944 never happened. One star from 1944 that never happened in this universe was the Martin-Baker MB.5. This remarkable fighter flew as a prototype and demonstrated capabilities that left every other aircraft in the shade. This superb aircraft had everything going for it, apart from timing. We asked Dr RV Smith to tell its story.  

The Martin-Baker MB1 G-ADCS was a clean two seat low wing monoplane, which was built at Denham and first flown from nearby Northolt during March 1935. The company then turned its talents to the design of a series of high-performance fighter aircraft that set new standards for ease of maintenance and servicing. 

The MB2 (M-B-1/G-AEZD/P9594) first flew at Harwell on 3 August 1938; the MB3 R2492 first flew at Wing on 31 August 1942. Sadly, the MB3 crashed following engine failure on 12 September 1942 fatally injuring Capt. Baker.

Martin-Baker MB5

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The design of the MB3 was evolved into the Rolls-Royce Griffon-powered Martin-Baker MB5 R2496. This imposing aircraft featured a large contra-rotating propeller, wide undercarriage track, straight-tapered wing of 35ft span mounting four 20-mm Hispano cannon, and an under-fuselage radiator unit, similar to that of the Mustang.

The cockpit was set well-forward under a blown canopy, providing excellent all-round vision and forward view over the slim downward-sloping nose.

The MB5 was flown for the first time at Harwell on 23rd May 1944.

The MB5 R2496 was displayed publicly at Farnborough in October 1945 and in June 1946. The latter display, flown by Jan Zurakowski, was described as ‘presenting one of the most brilliant flying demonstrations of the day and was outstanding for its speed, range and manoeuvrability’. Zurakowski later said it was ‘the best airplane I have ever flown’.

The comments below have been summarised from a number of articles, several of which draw upon a 1946 report “A&AEE Report 838 Pt 1 MB5 Engineering & Maintenance appraisal”, which is held in the National Archives.

Philip Jarrett comments in an article for Rolls-Royce Magazine that ‘the A&AEE report praised the MB5 in unusually glowing terms, using a generous number of superlatives’.

Perhaps the most striking comments, which are quoted in the Flight Magazine flight test article published on 18th December 1947 and written by Wing Commander MA Smith, DFC state:

“… this aircraft is excellent and is greatly superior, from the engineering and maintenance aspect, than any similar type. The layout of the cockpit might very well be made standard for normal piston-engined fighters, and the engine installation might, with great advantage, be applied to other aircraft.”

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Other articles also quote the statement that “The time necessary for a quick turn-around… would appear to be very low when compared with existing types of aircraft.”

Jarrett expands on this with the following description: “The 2,340hp Rolls-Royce Griffon 83 engine with its de Havilland contra-rotating propeller was carried on a special mounting that made its removal simple, and all of the cowling panels were also quickly removable, laying the engine completely bare ‘within a few minutes’.

Access to the carburettor main auxiliary gearbox, ignition system and Coffman cartridge starter was easy. All of the coolant radiators were enclosed within the rear fuselage, using a common intake and a controllable efflux.

Likewise, the fuselage panels were quickly detachable, allowing immediate access to all parts of the aircraft’s structure and the accessories and equipment. Every strut or member of the tubular fuselage frame was easily accessible and simple to replace in the event of damage.

The cockpit layout was described as ‘excellent.’ Martin-Baker’s patented control assembly could be removed en bloc by withdrawing a few bolts, without affecting the control settings. All three instrument panels, one in the centre and two at the sides, hinged fully forward when two quick-release handles were undone, permitting instruments to be changed with the minimum of effort.

 

Quickly opened bays in the upper surfaces gave access to the two 20mm Hispano cannon in each wing, with 200 rounds per gun fed by a Martin-Baker flat-feed mechanism. A servicing platform could be attached to ease the armourer’s task.”

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The Martin-Baker MB5 had a 35 ft wingspan and was 37 ft 9 in long. The undercarriage track was 15ft 2in. The MB5 had a maximum speed of 395 mph at sea level, 425 mph at 6,000 ft and 460 mph at 20,000 ft. The aircraft stalled at 95 mph in the landing configuration.

The MB5 had a quoted initial rate of climb of 3,800 fpm and could reach 20,000 ft in 6.5 minutes and 34,000 ft in 15 minutes. The aircraft had an empty weight of 9,233lb, a normal weight of 11,500lb, and a maximum weight of 12,090 lb.

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Some points made in the most interesting flight test report published in Flight International in December 1947 are summarised below:

“I was impressed by the size and somewhat brutal appearance of the power section and, in fact, of the whole aircraft.” The “clean-cut business-like appearance” of the aircraft “and its ‘office’ were confidence-producing”.

The “wide undercarriage gives a stable feel on the ground”. The stroboscopic effect of the contraprops when taxying toward the sun was most distracting.

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There was a tremendous response to throttle and the aircraft was delightful on take-off. The throttle was smooth and responsive, but the propeller pitch lever was rather sensitive with large response to small movement. The engine was virtually vibration-free and the noise level in the cockpit was low. The pilot cruised the MB5 at 315 mph at 8,000ft using 4lb boost and 2,250 rpm, these settings being being somewhat lower than those recommended.

The spring tab controls were said to give an air of laziness in response, their balance was commendable, but with a feeling of slight sponginess being commented on. Elevators and ailerons were “light, without being over-light, although the stick pressure required for a slow roll at about 315 mph was rather more than I had expected”.

Approaching the stall with flaps down at 3,000ft, the controls became sloppy around 110 mph, the aircraft rolling away to the left at just over 100 mph.

Approaching the airfield in a fast descent to about 1,200ft, the ASI showed about 465mph “the aircraft felt as smooth and solid as one could wish”. Putting the airscrew into fine pitch preparatory to landing “was like putting on a hand brake”.

The landing sequence was described as follows: Flaps down at 160 mph, power to adjust rate of descent. At around 130mph, the aircraft was trying to adopt the landing attitude, but still with a good forward view. Cross the hedge at around 115mph, throttle right back and flare, small attitude adjustment and the aircraft “sat down and stayed down on three points in a satisfactory manner”.

“I decided that the handling of the M-B 5 was pleasing in every way and that another hour or two on it would be a very enjoyable experience”.

The only cockpit criticisms were that “the ignition switches under the left elbow did not seem well positioned”, and that “the trim indicators were small and not too easy to read near the left hip.”

“However, in all important aspects of equipment and control, the M-B 5 definitely sets a very high standard.”

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Could the Martin-Baker MB5 have been improved upon?

It seems clear that the aircraft was superlative in terms of maintenance accessibility and possessed an excellent cockpit layout, subject to the minor points noted by W/Cdr Smith in his test report for Flight International. General handling and control harmonisation was clearly very good, although both W/Cdr Smith and, apparently Eric ‘Winkle’ Brown, had some reservations about the crispness of the roll control.

Two aspects occur to me, The wing loading (wing area 262 Sq ft) was rather high at 46.1 lb/sq ft at 12,090 lb maximum weight, resulting in a stall speed close to 100 mph and possibly limiting sustained turning performance.

Comparable figures for other well-known aircraft are as follows: Tempest V at 11.500 lb 38 lb/sq ft; Spitfire FRXIVE at 8,475 lb 34.8 lb/sq ft; P-51D at 10,100 lb 43.3 lb/sq ft.

Given the high speeds attained, there might also be scope for the use of an improved aerofoil. The MB5 used the RAF34 wing section, which dated back to 1927, albeit with the excellent pedigree of being used on the DH88 Comet and the DH98 Mosquito.

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It is interesting to speculate that one of the Hawker aerofoils used on the Tempest and Sea Fury, might have reduced the type’s drag at high speed and/or increased its critical Mach number.

So, my imagination drifts in the direction of an MB5 fuselage, powerplant and cooling system married to a Hawker Tempest V (302 sq ft) wing, or, probably better, a Fury (280 sq ft) wing (less the port wing root oil cooler).

— Dr RV Smith, CEng, FRAeS

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The Supersonic Rotor Helicopter

Westland SSRH 02 lrg (1) (2).jpgToday, thanks to former Head of Future Projects at Westland Helicopters, Dr Ron Smith, we have gleaned further information on this intriguing, and potentially world-beating, project. 

“The Supersonic Rotor Helicopter. this was a project
completed by the long-term Future Project Office prior to my joining
Westland in October 1975. A report summarising the work was needed to
secure contract payment and I was tasked with pulling it together
(based on the work already conducted by others).

The SSRH proposition is based on the fact that if you increase the
rotor tip speed, the retreating blade stall boundary goes out to a
higher helicopter forward speed. (It’s a function of the ratio of
forward speed to tip speed, which is known as the Advance Ratio).

Suppose the tip speed is Mach 0.6 and at a particular blade loading
(think weight), the retreating blade limit is at an advance ratio of
0.3. That means that retreating blade stall will occur at Mach 0.18
(about 230 mph). In this case, the VNE might be say 210 mph (10%
margin).

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If you double the tip speed to M=1.2, you can, in principle, fly at the
same advance ratio at double the speed (roughly 400 mph).

The study report (early 1976) looked at the shock wave propagation
geometries and a relatively basic performance calculation, in the
context of various designs targeted at naval roles. A range of
different tip Mach numbers were studied. WG32 was one of the sample
layouts (looking at them now, it appears that single, twin and three
engine variants were schemed). As far as I can tell, they were not
allocated separate WG numbers.

The obvious potential issues would be external noise and high power
requirements. But, in principle, it ought to work.

Although I wrote the report, I was not involved with any customer
meetings, but the feedback I was given by the Research Director was
that both he and the customer were very pleased with the report.

This was a piece of research to examine feasibility and highlight risks
and issues. I would imagine that it was felt that there was too much
risk to go down this route when conventional helicopter solutions could
probably provide adequate operational performance with lower risk in a
shorter timescale.

(Studies had already been completed on WG26 (Multi-Role Fleet
Helicopter) which went on via WG31 (Sea King Replacement) and WG34 to
become EH101 / Merlin).

I was not involved in any of these airframe studies, other than some
limited supporting work that I contributed to, in respect of the stall
flutter analysis of what became the BERP rotor blade.”PtVgAtsk.jpg

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My favourite Spitfire #5 – Supermarine Spitfire P.R. Mk. XI


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In World War II, aerial photo reconnaissance was scientific — a rigorous and methodical observation of the enemy’s strength. The Photo Reconnaissance Spitfire became the chief Allied tool of this undertaking, alongside the de Havilland Mosquito. Allied aerial reconnaissance gave the Manhattan Project and Bletchley Park a run for their war-winning money for its scale and cleverness. Within this effort, the Supermarine Spitfire excelled as an intelligence-gathering machine whose pilots had a secretive, heroic job performed alone over enemy territory.

The Spitfire, born as a fighter, roared into this new role with alacrity. Before even the Battle of Britain it was serving the PR mission with aplomb. Cameras, with lenses wider than our heads, displaced guns. This brought extra capacity for missions eventually to Norwegian fjords, radar sites in occupied France, German industrial cities. Never glamorous in appearance, the P.R. Spits wore mostly grey-blue or dull pink paint schemes, like something from our stealthy era.

Pride of the Kriegsmarine, the battleship Bismarck, was spotted readying for her fatal high seas debut by a P.R. Spitfire pilot. The very last Royal Air Force operational flight by a Spitfire utilised a P.R. Version, in 1954! All the milestone editions of the Spitfire included camera-equipped versions. The P.R. Mark XI, in the very middle of the Spitfire line, is a wonderful thing. Look for camera ports, pointy fin and rudder and an enlargement to the underside of the nose for the bigger engine oil tank needed on those long, cold flights that helped win a war.

The Hush-Kit Book of Warplanes is a gorgeous heavily-illustrated – and often irreverent – coffee-table book covering the history of military aviation from 1914 – the present. Volume 2 is now crowd fund-raising through advanced pre-orders here.

Stephen Caulfield is a civilian employee of the Salvation Army “stationed” on the frontlines of North American consumer insanity in a modern recycling plant where he finds the occasional Spitfire.

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