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    Title :

    Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles


    Contributors:


    Publication date :

    2015




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik



    Shock-induced boundary layer separation in overexpanded conical exhaust nozzles

    Arens, M. / Spiegler, E. | Engineering Index Backfile | 1963


    Turbulent-flow separation criteria for overexpanded supersonic nozzles

    Marrisette, E. Leon / Goldberg, Theodore J. | TIBKAT | 1978


    Numerical Simulation of Shock/Boundary Layer Interaction in Supersonic Nozzles

    Perrot, Y. / Hadjadj, A. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2005



    Phenomenon of flow separation in overexpanded supersonic or rocket nozzles

    Vandenkerckhove, J. | Engineering Index Backfile | 1956