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. (Author)


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    Title :

    Scramjet Nozzle Design and Analysis as Applied to a Highly Integrated Hypersonic Research Airplane


    Contributors:

    Publication date :

    1976


    Size :

    46 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    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. P. / Small, W. J. / Penland, J. A. | NTRS | 1976