The response of a nominally two-dimensional transonic diffuser flow to abrupt downstream perturbations was examined experimentally.


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    Title :

    Terminal Shock Response in Ramjet Inlets to Abrupt Downstream Perturbations


    Contributors:
    M. Sajben (author) / T. J. Bogar (author)

    Publication date :

    1988


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    COMPRESSIBLE BOUNDARY LAYER INVESTIGATION FOR RAMJET/SCRAMJET INLETS AND NOZZLES

    Goldfeld, M. A. / AIAA | British Library Conference Proceedings | 2003


    COMPRESSIBLE BOUNDARY LAYER INVESTIGATION FOR RAMJET/SCRAMJET INLETS AND NOZZLES

    Goldfeld, M. A. / Starov, A. V. / Semenova, Y. V. | British Library Conference Proceedings | 2004