| Burst-mode frequency effects of dielectric barrier discharge plasma actuator for separation control S Sekimoto, T Nonomura, K Fujii AIAA Journal 55 (4), 1385-1392, 2017 | 94 | 2017 |
| Closed-Loop Flow Separation Control Using the Deep Q Network over Airfoil S Shimomura, S Sekimoto, A Oyama, K Fujii, H Nishida AIAA Journal 58 (10), 4260-4270, 2020 | 56 | 2020 |
| 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, 15-00233, 2015 | 46 | 2015 |
| A high-fidelity body-force modeling approach for plasma-based flow control simulations D Chen, K Asada, S Sekimoto, K Fujii, H Nishida Physics of Fluids 33 (3), 037115, 2021 | 23 | 2021 |
| Experimental Study on Application of Distributed Deep Reinforcement Learning to Closed-loop Flow separation Control over an Airfoil S Shimomura, S Sekimoto, A Oyama, K Fujii, H Nishida AIAA Scitech 2020 Forum, 0579, 2020 | 20 | 2020 |
| Flow-control capability of electronic-substrate-sized power supply for a plasma actuator S Sekimoto, K Fujii, S Hosokawa, H Akamatsu Sensors and Actuators A: Physical, 111951, 2020 | 18 | 2020 |
| An effective three-dimensional layout of actuation body force for separation control I Kaneda, S Sekimoto, T Nonomura, K Asada, A Oyama, K Fujii International Journal of Aerospace Engineering 2012, 2012 | 17 | 2012 |
| In-Flight Demonstration of Stall Improvement Using a Plasma Actuator for a Small Unmanned Aerial Vehicle S Sekimoto, H Kato, K Fujii, H Yoneda Aerospace 9 (3), 144, 2022 | 14 | 2022 |
| Dynamic burst actuation to enhance the flow control authority of plasma actuators T Ogawa, K Asada, S Sekimoto, T Tatsukawa, K Fujii Aerospace 8 (12), 396, 2021 | 14 | 2021 |
| Flow control around NACA0015 airfoil using a dielectric barrier discharge plasma actuator over a wide range of the Reynolds number S Sekimoto, K Fujii, M Anyoji, Y Miyakawa, S Ito, S Shimomura, H Nishida, ... Actuators 12 (1), 43, 2023 | 13 | 2023 |
| Comparative study of co-flow and counter blowing DBD plasma actuators for separated flow over an airfoil S Sekimoto, K Asada, M Anyoji, T Nonomura, K Fujii 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012 | 11 | 2012 |
| Experimental Study of Effects of Frequency for Burst Wave on a DBD Plasma Actuator for Separation S Sekimoto, T Nonomura, K Fujii 54th AIAA Aerospace Sciences Meeting, 0844, 2016 | 10 | 2016 |
| Experimental Analysis of Closed-Loop Flow Control Around Airfoil Using DBD Plasma Actuator S Shimomura, T Ogawa, S Sekimoto, T Nonomura, A Oyama, K Fujii, ... Fluids Engineering Division Summer Meeting 58066, V01CT22A004, 2017 | 9 | 2017 |
| Computational Study of Wing-Tip Effect for Flow-Control Authority of Dielectric-Barrier-Discharge Plasma Actuator T Abe, K Asada, S Sekimoto, K Fukudome, T Tatsukawa, H Mamori, ... AIAA Journal, 1-14, 2020 | 8 | 2020 |
| Aerodynamic drag reduction of a simplified vehicle model by promoting flow separation using plasma actuator K SHIMIZU, T NAKASHIMA, S SEKIMOTO, K FUJII, T HIRAOKA, ... Mechanical Engineering Letters 5, 19-00354-19-00354, 2019 | 8 | 2019 |
| Experimental study of a nano-second pulse plasma actuator for low Reynolds number flow control S Sekimoto, T Sulaiman, M Anyoji, T Nonomura, K Fujii 52nd Aerospace Sciences Meeting, 0767, 2014 | 8 | 2014 |
| DBD plasma actuator multi-objective design optimization at Reynolds number 63,000: baseline case T Sulaiman, S Sekimoto, T Tatsukawa, T Nonomura, A Oyama, K Fujii Fluids Engineering Division Summer Meeting 55553, V01BT15A007, 2013 | 7 | 2013 |
| Experimental Analysis of Burst Actuation for Separation Control around a Pitching NACA0015 Airfoil Using a DBD Plasma Actuator at low Reynolds number S Sekimoto, S Shimomura, H Fukumoto, K Fujii, A Oyama, H Nishida 2018 AIAA Aerospace Sciences Meeting, 1551, 2018 | 6 | 2018 |
| Study on the Sensing Parameters toward Better Feed-back Control of Stall Separation with DBD Plasma Actuator T Ogawa, S Shimomura, K Asada, S Sekimoto, T Tatsukawa, K Fujii, ... 35th AIAA Applied Aerodynamics Conference, 3565, 2017 | 6 | 2017 |
| Experimental Study of Burst Ratio Effect for Dielectric-Barrier-Discharge Plasma Actuator for Separation Control S Sekimoto, N Tanaka, T Nonomura, H Nishida, K Fujii 55th AIAA Aerospace Sciences Meeting, 1688, 2017 | 6 | 2017 |
Taku NonomuraDepartment of Aerospace Engineering, Graduate School of Engineering, Nagoya UniversityBestätigte E-Mail-Adresse bei mae.nagoya-u.ac.jp
