Youtube hearted comments of John Burns (@johnburns4017).
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Nice vid.
There is a myth that the Germans were way ahead of the British in jet engines and planes in WW2, when the opposite is true. The WW2 German jet engines were extremely unreliable with low performances and very high fuel consumption. The German axial-flow turbojets never worked as they wanted, being developed up to 1953 by the French to obtain a usable engine. The French lost a lot of time playing around with the German engines, instead of working with the British. The French and Soviets after WW2 tried to improve the German axial-flow engines and largely failed.
The Germans did not invent the axial-flow turbojet, they based everything on Frank Whittle's patents. The British Metropolitan-Vickers F.1 axial-flow engine was running on a test bed in 1941. The F.2 was an axial-flow being an extremely advanced design using a nine-stage axial compressor, annular combustor, and a two-stage turbine. It powered a Meteor in November 1943. It was considered unreliable and never saw use during the war, hence why the British went for the reliability, controllability and quick development of the centrifugal turbojets. The Metro-Vick F.3 was the first ever turbofan in 1943. Metro-Vick developed the F.9 Sapphire, however left the jet business in 1947 giving all their designs to Armstrong Siddeley, who commercially produced the Armstrong Siddeley Sapphire engine, which was licence built in the US as the J-65.
The British in order to get a usable and reliable jet engine, with the technology of the time, went for a centrifugal design rather than the troublesome axial-flow design. This design produced less thrust than an axial-flow but was quicker to develop and reliable outperforming the best piston engines planes at the time. It took 5 months to develop, while the first reliable axial-flow engine was the 1950 Rolls Royce Avon, which took 5 years to get right. The Avon is still in production as a ground based gas turbine, with the aero version in production for 30 years.
In 1945 the French made and tested some German designed turbo jets made with quality alloys developed by the British unavailable to German industry in WW2, as they never had a high temperature alloys project. They ran for 25 hours instead of the 10 hours of the Germans engines that used poorer quality alloys. Not much better. The German axial-flow engines failed because of heavy design flaws. The centrifugal compressor used by the first British Meteor plane was fine and much more reliable, but unable to reach high compression ratios. This limited performances. Centrifugal compressors were used up to the 1960s.
In 1945 the team from the French ATAR laboratory plus some BMW and Junkers engineers, were engaged by the French SNECMA research bureau, with the objective to build a new reliable and performing axial-flow turbojet. The BMW 003/Jumo004 was considered unusable. It was tested on the first French jet aircraft, the 1946 So6000 Triton, overheating and exploding. The plane only flew with a Rolls Royce Nene centrifugal turbojet.
The ATAR project took 6 years to produce the first acceptable axial-flow turbojet (ATAR 101 B1), produced in 1953. So 8 years research and developments by the French using the German jet engines as the base with also years of German research. It was installed on the first French jet fighter, the Dassault Ouragan.
The French lost a lot of time because the German jets had poor efficiency and some concept failures. The failures were essentially in the combustion chambers and fresh air circulation to reduce the external temperature of the engine. The BMW jet was known for overheating problems which precluded fuselage installation.
The question at the end of WW2 was: what is the most efficient way to produce jet fighters? The answer was clearly not adopting the German design of engine and fuselage. The build costs for a jet engine were much higher than a piston engine, with the fuel consumption near 3x. The centrifugal compressor the British adopted in some planes was the best choice with 1944-45 technology, more compression pressure was not an advantage when the hot turbine was unable to resist higher temperatures. The German turbojets had big overheat problems as the engine would not work in an enclosed fuselage for single-engined fighters. This defect was immediately noted by the French on the 1946 "SO 6000 Triton" prototype, and by the Soviets on the 1946 Mig 9. The Soviets quickly replaced the BMW 004B2 by the centrifugal Rolls Royce Nene which worked without problems, dismissing the BMW engine for fighter planes. The Rolls Royce Nene was copied to the last nut by the USSR being installed in the Mig 15 being used effectively in the Korean war.
The Meteor was the first proper fully developed jet plane introduced operationally. The me262 was with a testing unit until November 1944. The 262 was slightly faster than the Meteor F3, but extremely unreliable. The British would never put into the sky such an undeveloped plane as the me262. The British could have had a jet fighter operational in 1941, but it may have been as bad as the me262. The Germans advanced R&D on jets after they interrogated captured British RAF men. They learned the British were advanced in jet technology and flying prototype planes. Until then the Germans had no intention of mass producing jet planes.
The rushed together Me262 started claiming kills on 26 July 1944, the Meteor claimed its first V1 kill a few days later on the 4 August 1944. But the Meteor was a proper fully developed jet plane, not a thrown together desperate effort as the me262 was. The me262 fuselage was similar to a piston plane with the pilot over the wings obscuring downward vision, while the Meteor was a proper new design fuselage specifically for jet fighters with a forward of the wings pilot position giving superior pilot vision, as we see in planes today. The cockpit was very quiet. The Meteor was built to known aerodynamics so if problem it could be pinned to the new jet engine. The Meteor during WW2 was having more advanced engines fitted as they were being released and changes to the nacelles.
The sweptback wings of the me262 were to move the engines further back for better weight distribution, not for aerodynamic reasons as is thought the case. The me262's airframe was based on piston engine planes, even with an initial rear tail wheel. The tricycle landing gear was only introduced when it was found the thrust of the jet engines would scorch the runway surface as the exhaust faced downwards. The Meteor's airframe was designed purely for jet propulsion even with a high tail to prevent thrust interfering with the tail which could affect control.
Only the manufacturer claimed 550mph from the me262. No one ever reached that intentionally. German pilots were instructed not go over 450mph as the airframe would react unpredictably with the engine in danger of blowing. 450mph was only a few mph faster than the Spitfire Mk XIV.
The Meteor is still flying today being flown operationally until the 1980s, being used by many countries. Unlike the the 262, which apart from the Czechs using them for a few years after WW2, no one bothered with.
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