Discussion directed toward power plants for sophisticated multipurpose strike aircraft, with reference to optimum use of lift/ thrust engine concept in its extended form, where extra thrust is obtained by burning fuel in bypass air stream prior to its discharge from nozzles; review of thermodynamic characteristics required of engines for future "vectored thrust", low level, strike aircraft having supersonic capability; relative merits of extreme forms of power plant are discussed from engine and power plant designer's viewpoint.


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    Titel :

    Extensions of lift/thrust engine principle in V/STOL aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Denning, R.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Fighter



    Erscheinungsdatum :

    1962


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Extensions of the Lift/Thrust Engine Principle in V/STOL Aircraft

    Denning, R. M. | SAE Technical Papers | 1962


    Optimum Lift/Thrust System for V/STOL Aircraft

    Dev, S.P. | British Library Conference Proceedings | 2008


    Lift-thrust turbofan engines for VTOL and STOL aircraft

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


    Lift-Thrust Turbofan Engines for VTOL and STOL Aircraft

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