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    Transonic flow in the throat region of axisymmetric nozzles

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

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

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

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

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

    Nonuniform nozzle flow effects on base pressure at supersonic flightspeeds

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

    Swirling supersonic nozzle flow

    DUTTON, J. C. | AIAA | 1987

    Effects of a base cavity on subsonic near-wake flow

    KRUISWYK, R. W. / DUTTON, J. C. | AIAA | 1990

    Investigation of supersonic mixing layers

    RENIE, J. P. / DUTTON, J. C. / KRIER, H. et al. | AIAA | 1990

    Multiple normal shock wave/turbulent boundary-layer interactions

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

    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

    Three-dimensional velocity field in a compressible mixing layer

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

    Computations and experiments for a multiple normal shock/boundary-layer interaction

    CARROLL, B. F. / LOPEZ-FERNANDEZ, P. A. / DUTTON, J. C. | AIAA | 1993

    Effects of Afterbody Boattailing on the Near-Wake of Axisymmetric Bodies in Supersonic Flow

    Herrin, J. L. / Dutton, J. C. / AIAA | British Library Conference Proceedings | 1994

      Effects of Afterbody Boattailing on the Near-Wake of Axisymmetric Bodies in Supersonic Flow

      Herrin, J. L. / Dutton, J. C. / AIAA | British Library Conference Proceedings | 1994