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Between 1936 and 1940 Alan Arnold Griffith designed a series of turbine engines that were built under the direction of Hayne Constant at the Royal Aircraft Establishment (RAE). The designs were advanced for the era, typically featuring a "two-spool" layout with high- and low-pressure compressors that individually had more stages than typical engines of the era. Although advanced, the engines were also difficult to build, and only the much simpler "Freda" design would ever see production, as the Metrovick F.2 and later the Armstrong Siddeley Sapphire. Much of the pioneering work would be later used in Rolls-Royce designs, starting with the hugely successful Rolls-Royce Avon.
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that were built under the direction of Hayne Constant atthe Royal Aircraft Establishment (RAE). The designs were advanced for the era, typically featuring...
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invented theturbojet engine. A patent was submitted by Maxime Guillaume in 1921 for a similar invention which was technically unfeasible atthe time. Whittle's...
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with four de Havilland Ghost turbojet engines buried in the wing roots, a pressurised cabin, and large windows. For the era, it offered a relatively quiet...
TheRAE approached Armstrong Siddeley with an offer to help with the design, both to improve the F.2 and to get the company familiar with turbojet design...
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up atR.A.E. Bedford. The two-seat 707C joined theR.A.E. in January 1956; perhaps its most substantial research contribution was to thedevelopment of...
published. In it he talks about the needs for high-speed flight and the use of turbojets as the only reasonable solution to the problem of propeller efficiency...
thrust. However, development of the Saturn was cancelled; in its place, the more capable but not immediately available Bristol Orpheus turbojet engine was adopted...
turbojets with variable engine intake ramps, and reheat for take-off and acceleration to supersonic speed. Constructed out of aluminium, it was the first...
of the first to develop a strong theoretical basis for the jet engine. Griffith's advanced axial-flow turbojet engine designs were integral in the creation...
The aircraft had reliability problems because of strategic materials shortages and design compromises with its Junkers Jumo 004 axial-flow turbojet engines...
air intake located where the Pika's cockpit was. The Jindivik Mk.1 was powered by an Armstrong Siddeley Adder (ASA.1) turbojet, which had been developed...
fighters in the process. Atthe time, there was no conventional means for aircraft designers to meet these goals; the new Junkers Jumo 004B turbojets could...