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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lift-thrust turbofan engines for VTOL and STOL aircraft


    Weitere Titelangaben:

    Aeroplane Astronautics


    Beteiligte:
    Young, P.H.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Lift-Thrust Turbofan Engines for VTOL and STOL Aircraft

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


    Lift-thrust turbofan engines for VTOL and STOL aircraft

    Young, P.H.J. | Engineering Index Backfile | 1961


    Lift/thrust engines for VTOL aircraft

    Engineering Index Backfile | 1961


    VTOL-STOL aircraft

    Engineering Index Backfile | 1956