Concord supersonic transport will be powered by 4 Olympus 593 turbojet engines; Bristol Siddeley will provide turbojets; jet pipe; propulsive nozzles, reversers and silencers are SNECMA contribution; choice of optimum-cycle engine for supersonic aircraft is compromise; maximum thrust is required at takeoff, during transonic acceleration and when cruising; at same time low consumption is essential while cruising and during considerable time at subsonic speeds; development problems involved; Concord flight plan; problems raised by intake and exhaust system.


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    Titel :

    Concord propulsion


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Hooker, S.G. (Autor:in) / Garnier, M.M. (Autor:in)

    Erschienen in:

    Flight ; 85 , n 2876


    Erscheinungsdatum :

    1964


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Concord progress

    Edwards, G. | Engineering Index Backfile | 1964


    Concord progress

    Edwards, G. | Engineering Index Backfile | 1964


    Concord progress

    Edwards, G. | Engineering Index Backfile | 1964


    Progress with "concord"

    Engineering Index Backfile | 1966


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    Engineering Index Backfile | 1963