Personnel from NASA Lewis Research Center spoke on the subject of inlet duct and nozzle high speed validation experiments to include crossing shocks and boundary layer interaction, unsteady shock/boundary layer interactions, and vortex generators. Attention was also paid to the subjects of high speed mixing and transition ducts. Specific application was made to the NASP hypermixing concepts.


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    Title :

    NASA. Lewis Research Center/IFMD inlet duct and nozzle high speed validation experiments


    Contributors:


    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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    RATAJCZAK, A. / BIFANO, W. / MARTZ, J. et al. | AIAA | 1978