A global method of data reduction applied to seven-hole probes von Benay, R.

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Shock Wave/Transitional Boundary-Layer Interactions in Hypersonic Flow von Benay, R, Chanetz, B, Mangin, B, Vandomme, L, Perraud, J

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Experimental and numerical study of forced shock-wave oscillations in a transonic channel von Bur, R., Benay, R., Galli, A., Berthouze, P.

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Optimization of Viscous Waveriders Derived from Axisymmetric Power-Law Blunt Body Flows von Mangin, B, Benay, R, Chanetz, B, Chpoun, A

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Design of a boundary layer suction device for a supersonic quiet wind tunnel by numerical simulation von Benay, R., Chanetz, B.

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Modeling of Controlled Shock-Wave/Boundary-Layer Interactions in Transonic Channel Flow von Benay, Richard, Berthouze, Pascal, Bur, Reynald

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Shock unsteadiness creation and propagation: experimental analysis von Benay, R., Alaphilippe, M., Severac, N.

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Investigation of shock waves interference and associated hysteresis effect at variable-Mach-number upstream flow von Durand, A., Chanetz, B., Benay, R., Chpoun, A.

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Experimental and numerical study of the Mars Pathfinder vehicle von Bur, R., Benay, R., Chanetz, B., Galli, A., Pot, T., Hollis, B., Moss, J.

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Experimental and numerical study of the laminar separation in hypersonic flow von Chanetz, B, Benay, R, Bousquet, J.-M, Bur, R, Pot, T, Grasso, F, Moss, J

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Two-equation k-σ turbulence model : Application to a supersonic base flow von BENAY, Richard, SERVELT, Patrick

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Overview of Neonatal Lupus von Johnson, Benay, MSN, RN, CPNP, NNP-BC

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Optimizationof viscous Waveriders Derived from Axisymmetric Power-Law Blunt Body Flows von Mangin, B, Benay, R, Chanetz, B, Chpoun, A

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Comparison between methods of generation of waveriders derived from conical flows von Mangin, Bruno, Chpoun, Amer, Benay, Richard, Chanetz, Bruno

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Code verification/validation with respect to experimental data banks von Benay, Richard, Chanetz, Bruno, Délery, Jean

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Modeling of controlled shock-wave/boundary-layer interactions in transonic channel flow von Benay, R., Berthouze, P., Bur, R.

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Modeling of Afterbody Flows with Realistic Propulsive Gases: A Prospective Study von Benay, Richard, Servel, Patrick

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The HART II test – measurement of helicopter rotor wakes von van der Wall, Berend G, Burley, Casey L, Yu, Yung, Richard, Hugues, Pengel, Kurt, Beaumier, Philippe

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Shock wave/turbulent boundary layer interaction in the flow field of a tri-dimension wind tunnel von Benay, R., Pot, T.

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A Study of Turbulence Modelling in Transonic Shock-Wave Boundary-Layer Interactions von Benay, R., Cöet, M.-C., Délery, J.

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