Dynamic stall control using deployable leading-edge vortex generators A Le Pape, M Costes, F Richez, G Joubert, F David, JM Deluc
AIAA journal 50 (10), 2135-2145, 2012
94 2012 High-resolution computational fluid dynamics predictions for the static and dynamic stall of a finite-span OA209 wing R Jain, A Le Pape, A Grubb, M Costes, F Richez, M Smith
Journal of Fluids and Structures 78, 126-145, 2018
52 2018 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 Numerical investigation of three-dimensional static and dynamic stall on a finite wing K Kaufmann, M Costes, F Richez, AD Gardner, AL Pape
Journal of the American Helicopter Society 60 (3), 1-12, 2015
38 2015 Selective frequency damping method for steady RANS solutions of turbulent separated flows around an airfoil at stall F Richez, M Leguille, O Marquet
Computers & Fluids 132, 51-61, 2016
36 2016 Numerical investigation of three-dimensional effects during dynamic stall M Costes, F Richez, A Le Pape, R Gavériaux
Aerospace Science and Technology 47, 216-237, 2015
34 2015 Analysis of dynamic stall mechanisms in helicopter rotor environment F Richez
Journal of the American Helicopter Society 63 (2), 1-11, 2018
33 2018 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
31 2008 Zonal detached-eddy simulation of separated flow around a finite-span wing F Richez, A Le Pape, M Costes
AIAA Journal 53 (11), 3157-3166, 2015
30 2015 Algebraic Nonlocal Transition Modeling of Laminar Separation Bubbles Using L Bernardos, F Richez, V Gleize, GA Gerolymos
AIAA Journal 57 (2), 553-565, 2019
29 2019 Zonal detached-eddy simulation of an airfoil in poststall condition A Le Pape, F Richez, S Deck
AIAA journal 51 (8), 1919-1931, 2013
23 2013 The CREATION project for rotorcraft concepts evaluation: The first steps PM Basset, A Tremolet, F Cuzieux, C Schulte, D Tristrant, T Lefebvre, ...
20 2011 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
19 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
18 2019 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 Assessment of laminar-turbulent transition modeling methods for the prediction of helicopter rotor performance F Richez, A Nazarians, C Lienard
43rd European rotorcraft Forum, Milan, Italy, 2017
14 2017 Bifurcation scenario for a two-dimensional static airfoil exhibiting trailing edge stall D Busquet, O Marquet, F Richez, M Juniper, D Sipp
Journal of Fluid Mechanics 928, A3, 2021
13 2021 A numerical analysis of the dynamic stall mechanisms on a helicopter rotor from light to deep stall C Castells, F Richez, M Costes
Journal of the American Helicopter Society 65 (3), 1-17, 2020
13 2020 Validation of boundary-layer-transition computations for a rotor with axial inflow K Kaufmann, P Ströer, F Richez, C Lienard, P Gardarein, N Krimmelbein, ...
75th Annual Forum and Technology Display, 2019
13 2019 Numerical analysis of dynamic stall for different helicopter rotor flight conditions F Richez
Proceedings of the 73rd Annual Forum of the American Helicopter Society, 2017
13 2017