Propelling nozzle is required to operate at high efficiency over wide range of conditions -- typically five to ten-fold variation of exhaust pressure ratio; problems of geometry which such requirements entail are considered and reasons are given which show that nozzle of center-body form with parallel outer shroud appears attractive solution; in support of claims for this arrangement of nozzle, test data are presented from both single and twin models under representative conditions of external flow.


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    Titel :

    Centre-body nozzles for supersonic transport aircraft


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Herbert, M.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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