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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    Titel :

    Integration of Turbo-Ramjet Engines for Hypersonic Aircraft


    Beteiligte:
    O. Herrmann (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    7 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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