| Improved two-dimensional dynamic stall prediction with structured and hybrid numerical methods K Richter, A Le Pape, T Knopp, M Costes, V Gleize, AD Gardner Journal of the American Helicopter Society 56 (4), 1-12, 2011 | 91 | 2011 |
| Transition and turbulence modeling B Aupoix, D Arnal, H Bézard, B Chaouat, F Chedevergne, S Deck, ... AerospaceLab Journal, 1-13, 2011 | 54 | 2011 |
| DNS database of a transitional separation bubble on a flat plate and application to RANS modeling validation C Laurent, I Mary, V Gleize, A Lerat, D Arnal Computers & Fluids 61, 21-30, 2012 | 43 | 2012 |
| Near stall simulation of the flow around an airfoil using zonal RANS/LES coupling method F Richez, I Mary, V Gleize, C Basdevant Computers & Fluids 37 (7), 857-866, 2008 | 40 | 2008 |
| Reynolds-averaged Navier–Stokes simulations on NACA0012 and ONERA-M6 wing with the ONERA elsA solver J Mayeur, A Dumont, D Destarac, V Gleize AIAA Journal 54 (9), 2671-2687, 2016 | 29 | 2016 |
| Zonal RANS/LES coupling simulation of a transitional and separated flow around an airfoil near stall F Richez, I Mary, V Gleize, C Basdevant Theoretical and Computational Fluid Dynamics 22, 305-315, 2008 | 29 | 2008 |
| Improved Navier-Stokes computations of a stall-regulated wind turbine using low Mach number preconditioning A Le Pape, V Gleize 44th AIAA Aerospace Sciences Meeting and Exhibit, 1502, 2006 | 29 | 2006 |
| Multiple scale modeling of turbulent nonequilibrium boundary layer flows V Gleize, R Schiestel, V Couaillier Physics of Fluids 8, 2716, 1996 | 28 | 1996 |
| Algebraic Nonlocal Transition Modeling of Laminar Separation Bubbles Using Turbulence Models L Bernardos, F Richez, V Gleize, GA Gerolymos AIAA Journal 57 (2), 553-565, 2019 | 26 | 2019 |
| Grid sensitivity study for the turbulent viscous flow around a NACA0015 airfoil at stall M Costes, V Gleize, J Szydlowski, L Sankar, G Guzel, M Rhee | 25 | 2005 |
| Numerical and physical analysis of the turbulent viscous flow around a NACA 0015 profile at stall V Gleize, J Szydlowski, M Costes ONERA: Tire a Part, 1-20, 2004 | 24 | 2004 |
| RANS simulations on TMR 3D test cases with the Onera elsA flow solver J Mayeur, A Dumont, V Gleize, D Destarac 54th AIAA Aerospace Sciences Meeting, 1357, 2016 | 22 | 2016 |
| Numerical investigation of laminar/turbulent transition effects on the dynamic stall of an oscillating airfoil M Costes, V Gleize, A Le Pape, F Richez American Helicopter Society 4th Decennial Specialist’s Conference on …, 2008 | 21 | 2008 |
| Numerical simulation of a pitching airfoil under dynamic stall conditions including laminar/turbulent transition V Gleize, M Costes, A Le Pape, F Richez 46th AIAA Aerospace Sciences Meeting and Exhibit, 391, 2008 | 18 | 2008 |
| Prediction of separation-induced transition on the SD7003 airfoil using algebraic transition triggering L Bernardos, F Richez, V Gleize, GA Gerolymos AIAA Journal 57 (9), 3812-3824, 2019 | 16 | 2019 |
| Low-Mach-number preconditioning applied to turbulent helicopter fuselage flowfield computation V Gleize, M COSTES AIAA journal 41 (4), 653-662, 2003 | 16 | 2003 |
| Verification and validation of the Onera elsA flow solver on RANS benchmarks L Cambier, V Gleize, M Julien 52nd Aerospace Sciences Meeting, 0239, 2014 | 13 | 2014 |
| RANS simulations on TMR test cases and M6 wing with the Onera elsA flow solver J Mayeur, A Dumont, D Destarac, V Gleize AIAA Paper 1745, 2015, 2015 | 12 | 2015 |
| Low Mach Number Preconditioning for Unsteady Flow in General" ALE" Formulation V Gleize, A Le Pape 44th AIAA Aerospace Sciences Meeting and Exhibit, 687, 2006 | 12 | 2006 |
| RANS modeling of laminar separation bubbles around airfoils at low Reynolds conditions LF Bernardos, F Richez, V Gleize AIAA Aviation 2019 Forum, 2922, 2019 | 9 | 2019 |
Francois RichezResearch ScientistVerified email at onera.fr
