General analysis of problem for fighter aircraft indicate that with design maximum level flight Mach Number of 1.5 at 35,000 ft and given military load, power plant configuration resulting in lesser gross weight, and hence cost, is basic engine without afterburning. (see also Aeroplane v 85 n 2199 Sept 11 1953 p 393-6)


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    Titel :

    Afterburners -- Are they worth while?


    Weitere Titelangaben:

    Aeronautical Eng Rev


    Beteiligte:
    Newton, F.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1953


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Afterburners -- Are they worth while?

    Newton, F.C. | Engineering Index Backfile | 1953


    Afterburners

    Oates, Gordon C. | AIAA | 1985


    Afterburners for turbojet engines

    Cleveland, F.A. | Engineering Index Backfile | 1948


    Afterburners and variable nozzles

    Kress, R. | Engineering Index Backfile | 1952


    Afterburners and Variable Nozzles

    Kress, Ralph | SAE Technical Papers | 1953