Engine-nozzle airframe integration at hypersonic speeds was conducted by using a high-speed research aircraft concept as a focus. Recently developed techniques for analysis of scramjet-nozzle exhaust flows provide a realistic analysis of complex forces resulting from the engine-nozzle airframe coupling. By properly integrating the engine-nozzle propulsive system with the airframe, efficient, controlled and stable flight results over a wide speed range.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane


    Beteiligte:
    Small, W. J. (Autor:in) / Weidner, J. P. (Autor:in) / Johnston, P. J. (Autor:in)

    Erscheinungsdatum :

    1976-11-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane

    Small, William J. / Weidner, John P. / Johnston, P. J. | TIBKAT | 1976



    Scramjet integration on hypersonic research airplane concepts

    WEIDNER, J. / SMALL, W. / PENLAND, J. | AIAA | 1976