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