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 Soc Automotive Engrs -- Paper n 104 for meeting Apr 2-5 1957 8 p)


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    Title :

    Ramjet-Turbojet propulsion system for supersonic flight


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:


    Publication date :

    1957


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :