| Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number M Sato, T Nonomura, K Okada, K Asada, H Aono, A Yakeno, Y Abe, ... Physics of Fluids 27 (11), 2015 | 123 | 2015 |
| Geometric interpretations and spatial symmetry property of metrics in the conservative form for high-order finite-difference schemes on moving and deforming grids Y Abe, T Nonomura, N Iizuka, K Fujii Journal of Computational Physics 260, 163-203, 2014 | 76 | 2014 |
| A new technique for freestream preservation of finite-difference WENO on curvilinear grid T Nonomura, D Terakado, Y Abe, K Fujii Computers & Fluids 107, 242-255, 2015 | 72 | 2015 |
| Stable, non-dissipative, and conservative flux-reconstruction schemes in split forms Y Abe, I Morinaka, T Haga, T Nonomura, H Shibata, K Miyaji Journal of Computational Physics 353, 193-227, 2018 | 44 | 2018 |
| Conservative metric evaluation for high-order finite difference schemes with the GCL identities on moving and deforming grids Y Abe, N Iizuka, T Nonomura, K Fujii Journal of Computational Physics 232 (1), 14-21, 2013 | 40 | 2013 |
| Massive parametric study by LES on separated-flow control around airfoil using DBD plasma actuator at Reynolds number 63,000 M Sato, K Okada, T Nonomura, H Aono, A Yakeno, K Asada, Y Abe, ... 43rd AIAA fluid dynamics conference, 2750, 2013 | 35 | 2013 |
| On the freestream preservation of high-order conservative flux-reconstruction schemes Y Abe, T Haga, T Nonomura, K Fujii Journal of Computational Physics 281, 28-54, 2015 | 34 | 2015 |
| Control mechanism of plasma actuator for separated flow around NACA0015 at Reynolds number 63,000-separation bubble related mechanisms T Nonomura, H Aono, M Sato, A Yakeno, K Okada, Y Abe, K Fujii 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2013 | 29 | 2013 |
| High-order accurate direct numerical simulation of flow over a MTU-T161 low pressure turbine blade AS Iyer, Y Abe, BC Vermeire, P Bechlars, RD Baier, A Jameson, ... Computers & Fluids 226, 104989, 2021 | 22 | 2021 |
| Effects of fiber properties on aerodynamic performance and structural sizing of composite aircraft wings S Date, Y Abe, T Okabe Aerospace Science and Technology 124, 107565, 2022 | 17 | 2022 |
| Separated flow control of small horizontal-axis wind turbine blades using dielectric barrier discharge plasma actuators H Aono, H Fukumoto, Y Abe, M Sato, T Nonomura, K Fujii Energies 13 (5), 1218, 2020 | 14 | 2020 |
| Dominant parameters for maximum velocity induced by body-force models for plasma actuators S Kawai, T Bouwhuis, Y Abe, A Yakeno, T Nonomura, H Aono, A Oyama, ... Theoretical and Computational Fluid Dynamics 32, 805-820, 2018 | 13 | 2018 |
| Flow control using a DBD plasma actuator for horizontal-axis wind turbine blades of simple experimental model H Aono, Y Abe, M Sato, A Yakeno, K Okada, T Nonomura, K Fujii The 11th World Congress on Computational Mechanics, 20-25, 2014 | 13 | 2014 |
| Symmetric-conservative metric evaluations for higher-order finite difference scheme with the GCL identities on three-dimensional moving and deforming mesh Y Abe, N Iizuka, T Nonomura, K Fujii Proceedings of the 7th International Conference on Computational Fluid …, 2012 | 13 | 2012 |
| Flow characteristics around extremely low fineness-ratio circular cylinders M Kuwata, Y Abe, S Yokota, T Nonomura, H Sawada, A Yakeno, K Asai, ... Physical Review Fluids 6 (5), 054704, 2021 | 12 | 2021 |
| The effects of actuation frequency on the separation control over an airfoil using a synthetic jet Y Abe, K Okada, T Nonomura, K Fujii Progress in Flight Physics–Volume 7 7, 147-168, 2015 | 10 | 2015 |
| A new technique for finite difference WENO with geometric conservation law T Nonomura, Y Abe, K Fujii 21st AIAA Computational Fluid Dynamics Conference, 2569, 2013 | 9 | 2013 |
| Conservative high-order flux-reconstruction schemes on moving and deforming grids Y Abe, T Haga, T Nonomura, K Fujii Computers & Fluids 139, 2-16, 2016 | 8 | 2016 |
| Computational study on aeroacoustic fields of a transitional supersonic jet T Nonomura, Y Ozawa, Y Abe, K Fujii The Journal of the Acoustical Society of America 149 (6), 4484-4502, 2021 | 7 | 2021 |
| Unsteady shear layer flow under excited local body-force for flow-separation control in downstream of a two-dimensional hump A Yakeno, Y Abe, S Kawai, T Nonomura, K Fujii International Journal of Heat and Fluid Flow 74, 15-27, 2018 | 6 | 2018 |
