The integration of turbo-ramjet engines for hypersonic transport vehicles operating in the Mach 0 to 6+ regime represents one of the most important development tasks. A survey over the variety of interacting problem areas and faculties, which have to be integrated to lead to an optimized propulsion/airframe system, is presented


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    Title :

    Integration of Turbo-Ramjet Engines for Hypersonic Aircraft


    Contributors:
    O. Herrmann (author)

    Publication date :

    1992


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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