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    Two-stream, supersonic, wake flowfield behind a thick base. I - General features

    AMATUCCI, V. A. / DUTTON, J. C. / KUNTZ, D. W. et al. | AIAA | 1992

    Transonic flow in the throat region of axisymmetric nozzles

    DUTTON, J. C. / ADDY, A. L. | AIAA | 1981

    Time-Correlated Visualizations of Supersonic Blunt-Base Cylinder Wakes

    Kastengren, A. L. / Dutton, J. C. / Elliott, G. S. et al. | British Library Conference Proceedings | 2005

    Three-dimensional velocity field in a compressible mixing layer

    GRUBER, MARK R. / MESSERSMITH, NATHAN L. / DUTTON, J. C. | AIAA | 1993

    Swirling supersonic nozzle flow

    DUTTON, J. C. | AIAA | 1987

    Recompression Shock Unsteadiness in Supersonic Blunt-Base Cylinder Wakes

    Kastengren, A. L. / Dutton, J. C. / Elliott, G. S. et al. | British Library Conference Proceedings | 2005

    Pressure recovery in a constant-area, two-stream supersonic diffuser

    AMATUCCI, V. A. / ADDY, A. L. / DUTTON, J. C. | AIAA | 1982

    Passive Control of High-Speed Separated Flows Using Splitter Plates

    Reedy, T M | Online Contents | 2012
    Beteiligte: Dutton, J C

    Nonuniform nozzle flow effects on base pressure at supersonic flightspeeds

    ADDY, A. L. / DUTTON, J. C. / AMATUCCI, V. A. | AIAA | 1986

    Multiple normal shock wave/turbulent boundary-layer interactions

    CARROLL, BRUCE F. / DUTTON, J. C. | AIAA | 1992

    Multiple ducted streams with a periodic or a steady supersonic driver flow

    PETRIE, H. L. / ADDY, A. L. / DUTTON, J. C. | AIAA | 1985