Design and development of power-plant which is combination of conventional front mounted turbofan engine with system of rapidly rotatable exhaust nozzles; development of Bristol Siddeley BS 53, basic considerations, and thermodynamic parameters which fix engine design are turbine entry temperature at take-off, h-p compressor pressure ratio, bypass and fan pressure ratio; application of engine to single-engined V/STOL fighting aircraft for subsonic and supersonic roles. (See also SAE -- Paper 337A for meeting Apr 4-7 1961 10 p)
Lift-thrust turbofan engines for VTOL and STOL aircraft
Aeroplane Astronautics
Aeroplane and Astronautics ; 100 , n 2583
1961
3 pages
Aufsatz (Zeitschrift)
Englisch
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Lift-Thrust Turbofan Engines for VTOL and STOL Aircraft
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