Engine thrust and fuel consumption were determined for a wide range of simulated flight conditions and tail-pipe fuel flows. For standard TG-180 engine, the thrust was increased 109% by tail-pipe burning when investigated under conditions corresponding to Mach 1.18 at simulated altitude of 30,000 feet. Specific fuel consumption increased 67% above specific fuel consumption for standard engine without tail-pipe burning. General trends of experimental values agreed with values calculated from theoretical equations.


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    Titel :

    Altitude-Wind-Tunnel Investigations of Thrust Augmentation of a Turbojet Engine. 1 - Performance with Tail-Pipe Burning


    Beteiligte:
    A.W Fleming (Autor:in) / O.R Dietz (Autor:in)

    Erscheinungsdatum :

    1946


    Format / Umfang :

    60 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch