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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    Title :

    Ramjet-Turbojet propulsion system for supersonic flight


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1957



    Publication date :

    1957


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :