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 abstract in Aeroplane and Astronautics v 100 n 2583 Apr 20 1961 p 428-30)


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    Title :

    Lift-thrust turbofan engines for VTOL and STOL aircraft


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1961



    Publication date :

    1961


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Lift-Thrust Turbofan Engines for VTOL and STOL Aircraft

    Young, P. H. J. | SAE Technical Papers | 1961


    Control of Turbofan Lift Engines for VTOL Aircraft

    J. F. Sellers / J. R. Szuch | NTIS | 1973


    Lift/thrust engines for VTOL aircraft

    Engineering Index Backfile | 1961


    Control of turbofan lift engines for VTOL aircraft

    Sellers, J. F. / Szuch, J. R. | NTRS | 1973