Problem of pure jet aircraft take-off distance is indicated, and basic reasons for excess thrust deficiency as compared to propeller aircraft shown; afterburner concept discussed; thrust augmentations of 45% low speed and over 100% high speed shown to be feasible; method for analyzing afterburners. (See also - discussion n 9 Sept p 521)


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    Titel :

    Afterburners for turbojet engines


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1948


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    Summary of NACA Research on Afterburners for Turbojet Engines

    Fleming, W. A. / Gabriel, D. S. / Lundin, B. T. | NTRS | 1956


    Afterburners

    Oates, Gordon C. | AIAA | 1985


    THE METHODOLOGY OF COMBUSTION STABILITY OPTIMISATION IN TURBOJET AFTERBURNERS

    Chepkin, V. M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003


    Afterburners and variable nozzles

    Kress, R. | Engineering Index Backfile | 1952