The thrust, specific fuel consumption, and relative merits of the tandem fan and the dual reverse flow front fan propulsion systems for a supersonic V/STOL aircraft are discussed. Consideration is given to: fan pressure ratio, fan air burning, and variable core supercharging. The special propulsion system components required are described, namely: the deflecting front inlet/nozzle, the aft subsonic inlet, the reverse pitch fan, the variable core supercharger and the low pressure forward burner. The potential benefits for these unconventional systems are indicated.


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    Titel :

    Comparison of Two Parallel/Series Flow Turbofan Propulsion Concepts for Supersonic V/STOL


    Beteiligte:
    R. W. Luidens (Autor:in) / G. E. Turney (Autor:in) / J. Allen (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Optimizing the propulsion/lift system for turbofan STOL aircraft

    BOWLING, H. / HURKAMP, C. / THORNTON, R. | AIAA | 1969


    Optimizing the Propulsion/Lift System for Turbofan STOL Aircraft

    H. T. BOWLING / C. H. HURKAMP / AND R. M. THORNTON | AIAA | 1971