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.


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    Title :

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


    Contributors:

    Publication date :

    1976-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :




    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