Problem of applying propulsion system to supersonic aircrafts; it is shown that neither turbojets nor ramjets are entirely satisfactory when used by themselves; satisfactory results of combining two power plants into propulsion system; comparison of performance along operating altitude Mach number paths in terms of thrust and specific fuel consumption only. (see also abstract in Soc Automotive Engrs -- J v 65 n 8 July 1957 p 35-8)


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    Titel :

    Ramjet-Turbojet propulsion system for supersonic flight


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    de Vault, R.T. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1957



    Erscheinungsdatum :

    1957


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :