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Jean-Paul Dussauge

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Turbulent Boundary Layers In Subsonic And Supersonic Flow =
Turbulent Shear Layers in Supersonic Flow
Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA
Unsteady Effects of Shock Wave induced Separation
Transition Location Effect on Shock Wave Boundary Layer Interaction Experimental and Numerical Findings from the TFAST Project
Transition Location Effect on Shock Wave Boundary Layer Interaction Experimental and Numerical Findings from the TFAST Project
Unsteady Effects of Shock Wave Induced Separation
Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA