Comparative study of implicit and subgrid‐scale model large‐eddy simulation techniques for low‐Reynolds number airfoil applications DJ Garmann, MR Visbal, PD Orkwis
International Journal for Numerical Methods in Fluids 71 (12), 1546-1565, 2013
164 2013 Analysis of dynamic stall on a pitching airfoil using high-fidelity large-eddy simulations MR Visbal, DJ Garmann
AIAA Journal 56 (1), 46-63, 2018
148 2018 Three-dimensional flow structure and aerodynamic loading on a revolving wing DJ Garmann, MR Visbal, PD Orkwis
Physics of Fluids 25 (3), 2013
134 2013 Dynamics of revolving wings for various aspect ratios DJ Garmann, MR Visbal
Journal of Fluid Mechanics 748, 932-956, 2014
133 2014 Resume of the AIAA FDTC low Reynolds number discussion group's canonical cases M Ol, A Altman, J Eldredge, D Garmann, Y Lian
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010
87 2010 Numerical investigation of transitional flow over a rapidly pitching plate DJ Garmann, MR Visbal
Physics of Fluids 23 (9), 2011
77 2011 Experiments and computations on abstractions of perching K Granlund, M Ol, D Garmann, M Visbal, L Bernal
28th AIAA applied aerodynamics conference, 4943, 2010
66 2010 Dynamic stall of a finite-aspect-ratio wing MR Visbal, DJ Garmann
AIAA Journal 57 (3), 962-977, 2019
65 2019 Interactions of a streamwise-oriented vortex with a finite wing DJ Garmann, MR Visbal
Journal of Fluid Mechanics 767, 782-810, 2015
63 * 2015 Effect of sweep on dynamic stall of a pitching finite-aspect-ratio wing MR Visbal, DJ Garmann
AIAA Journal 57 (8), 3274-3289, 2019
52 2019 Resolvent analysis of an airfoil laminar separation bubble at CA Yeh, SI Benton, K Taira, DJ Garmann
Physical Review Fluids 5 (8), 083906, 2020
48 2020 Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation DJ Garmann
University of Cincinnati, 2013
47 2013 Numerical investigation of spanwise end effects on dynamic stall of a pitching NACA 0012 wing MR Visbal, DJ Garmann
55th AIAA aerospace sciences meeting, 1481, 2017
39 2017 Analysis of tip vortex near-wake evolution for stationary and oscillating wings DJ Garmann, MR Visbal
AIAA Journal 55 (8), 2686-2702, 2017
34 2017 High-fidelity simulations of afterbody vortex flows DJ Garmann, MR Visbal
AIAA Journal 57 (9), 3980-3990, 2019
30 2019 Effect of aspect ratio on finite-wing dynamic stall PR Hammer, DJ Garmann, MR Visbal
AIAA Journal 60 (12), 6581-6593, 2022
27 2022 Three-dimensional flow structure and aerodynamic loading on a low aspect ratio, revolving wing D Garmann, M Visbal
42nd AIAA fluid dynamics conference and exhibit, 3277, 2012
27 2012 High-fidelity simulations of dynamic stall over a finite-aspect-ratio wing MR Visbal, DJ Garmann
8th AIAA Flow Control Conference, 4243, 2016
24 2016 High-fidelity simulations of transitional flow over pitching airfoils D Garmann, M Visbal
39th AIAA Fluid Dynamics Conference, 3693, 2009
24 2009 Investigation of spanwise end effects on dynamic stall of a pitching wing section MR Visbal, DJ Garmann
Journal of Aircraft 56 (6), 2118-2130, 2019
23 2019 
Miguel VisbalAir Force Research LaboratoryZweryfikowany adres z us.af.mil
