| 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 | 157 | 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 | 132 | 2018 |
| Three-dimensional flow structure and aerodynamic loading on a revolving wing DJ Garmann, MR Visbal, PD Orkwis Physics of Fluids 25 (3), 2013 | 132 | 2013 |
| Dynamics of revolving wings for various aspect ratios DJ Garmann, MR Visbal Journal of Fluid Mechanics 748, 932-956, 2014 | 127 | 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 | 86 | 2010 |
| Numerical investigation of transitional flow over a rapidly pitching plate DJ Garmann, MR Visbal Physics of Fluids 23 (9), 2011 | 76 | 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 | 65 | 2010 |
| Interactions of a streamwise-oriented vortex with a finite wing DJ Garmann, MR Visbal Journal of Fluid Mechanics 767, 782-810, 2015 | 60* | 2015 |
| Dynamic stall of a finite-aspect-ratio wing MR Visbal, DJ Garmann AIAA Journal 57 (3), 962-977, 2019 | 55 | 2019 |
| Effect of sweep on dynamic stall of a pitching finite-aspect-ratio wing MR Visbal, DJ Garmann AIAA Journal 57 (8), 3274-3289, 2019 | 46 | 2019 |
| Characterization of the vortex formation and evolution about a revolving wing using high-fidelity simulation DJ Garmann University of Cincinnati, 2013 | 40 | 2013 |
| Resolvent analysis of an airfoil laminar separation bubble at CA Yeh, SI Benton, K Taira, DJ Garmann Physical Review Fluids 5 (8), 083906, 2020 | 37 | 2020 |
| 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 | 36 | 2017 |
| High-fidelity simulations of afterbody vortex flows DJ Garmann, MR Visbal AIAA Journal 57 (9), 3980-3990, 2019 | 29 | 2019 |
| Analysis of tip vortex near-wake evolution for stationary and oscillating wings DJ Garmann, MR Visbal AIAA Journal 55 (8), 2686-2702, 2017 | 29 | 2017 |
| 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 | 21 | 2019 |
| Effect of aspect ratio on finite-wing dynamic stall PR Hammer, DJ Garmann, MR Visbal AIAA Journal 60 (12), 6581-6593, 2022 | 20 | 2022 |
Miguel VisbalAir Force Research Laboratory在 us.af.mil 的电子邮件经过验证
