| 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 | 125 | 2015 |
| Multifactorial effects of operating conditions of dielectric-barrier-discharge plasma actuator on laminar-separated-flow control M Sato, H Aono, A Yakeno, T Nonomura, K Fujii, K Okada, K Asada AIAA journal 53 (9), 2544-2559, 2015 | 90 | 2015 |
| Modification of quasi-streamwise vortical structure in a drag-reduced turbulent channel flow with spanwise wall oscillation A Yakeno, Y Hasegawa, N Kasagi Physics of Fluids 26 (8), 2014 | 64 | 2014 |
| Computational and experimental analysis of flow structures induced by a plasma actuator with burst modulations in quiescent air H Aono, S Sekimoto, M Sato, A Yakeno, T Nonomura, K Fujii Mechanical Engineering Journal 2 (4), 15-00233-15-00233, 2015 | 44 | 2015 |
| Mechanisms for turbulent separation control using plasma actuator at Reynolds number of 1.6ื 106 M Sato, K Asada, T Nonomura, H Aono, A Yakeno, K Fujii Physics of Fluids 31 (9), 2019 | 43 | 2019 |
| 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 | 36 | 2013 |
| 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 |
| Separation control based on turbulence transition around a two-dimensional hump at different Reynolds numbers A Yakeno, S Kawai, T Nonomura, K Fujii International Journal of Heat and Fluid Flow 55, 52-64, 2015 | 24 | 2015 |
| 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 |
| Effective mechanisms for turbulent-separation control by DBD plasma actuator around NACA0015 at reynolds number 1,600,000 M Sato, K Asada, T Nonomura, H Aono, A Yakeno, K Fujii 7th AIAA Flow Control Conference, 2663, 2014 | 13 | 2014 |
| 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 |
| Drag reduction and transient growth of a streak in a spanwise wall-oscillatory turbulent channel flow A Yakeno Physics of Fluids 33 (6), 2021 | 11 | 2021 |
| Plasma flow control simulation of an airfoil of wind turbine at an intermediate Reynolds number H Aono, T Nonomura, A Yakeno, K Fujii, K Okada Fluids Engineering Division Summer Meeting 55553, V01BT15A008, 2013 | 11 | 2013 |
| Spatio-temporally periodic control for turbulent friction drag reduction A Yakeno, Y Hasegawa, N Kasagi Sixth International Symposium on Turbulence and Shear Flow Phenomena, 2009 | 11 | 2009 |
| Application of observability Gramian to targeted observation in WRF data assimilation R Yoshimura, A Yakeno, T Misaka, S Obayashi Tellus A: Dynamic Meteorology and Oceanography 72 (1), 1-11, 2020 | 10 | 2020 |
| Propagation of stationary and traveling waves in a leading-edge boundary layer of a swept wing A Yakeno, S Obayashi Physics of Fluids 33 (9), 2021 | 9 | 2021 |
| LES of Separated-flow Controlled by DBD Plasma Actuator around NACA 0015 over Reynolds Number Range of 10^ 4-10^ 6 M Sato, K Okada, H Aono, K Asada, A Yakeno, T Nonomura, K Fujii 53rd AIAA Aerospace Sciences Meeting, 0308, 2015 | 9 | 2015 |
| LES on turbulent separated flow around NACA0015 at Reynolds number 1,600,000 toward active flow control K Asada, M Sato, T Nonomura, S Kawai, H Aono, A Yakeno, K Fujii 32nd AIAA Applied Aerodynamics Conference, 2687, 2014 | 9 | 2014 |
| Mechanism of drag reduction by pre-determined spatio-temporally periodic control of wall turbulence A Yakeno, Y Hasegawa, N Kasagi Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of …, 2010 | 7 | 2010 |
Taku NonomuraDepartment of Aerospace Engineering, Graduate School of Engineering, Nagoya UniversityVerified email at mae.nagoya-u.ac.jp
