Metropolitan-Vickers F.2
aircraft engine model

The Metropolitan-Vickers F.2 is an early turbojet engine and the first British design to be based on an axial-flow compressor. It was an extremely advanced design for the era, using a nine-stage axial compressor, annular combustor, and a two-stage turbine.
It first powered a Gloster Meteor in November 1943, outperforming contemporary models from Power Jets. Despite this excellent start, it was considered unreliable and did not see use during the war. In the post-war era, newer engine designs provided much higher performance, and interest in the F.2 waned.
The potential of the engine and the investment did not go to waste, however; the design was passed from Metropolitan-Vickers (Metrovick) to Armstrong Siddeley when Metrovick left the gas turbine business. Armstrong Siddeley produced a larger version as the successful Sapphire.
Development
Alan Arnold Griffith published a seminal paper in 1926, An Aerodynamic Theory of Turbine Design, that for the first time clearly demonstrated that a gas turbine could be used as a practical, and even desirable, aircraft powerplant. The paper started by demonstrating that existing axial compressor designs were "flying stalled" due to their use of flat blades, and dramatic improvements could be made by using aerofoil designs instead. It went on to outline a complete compressor and turbine design, using the extra exhaust power to drive a second turbine that would power a propeller.
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