フォロー
Satoshi Sekimoto
Satoshi Sekimoto
確認したメール アドレス: go.tuat.ac.jp
タイトル
引用先
引用先
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
862017
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
472020
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
442015
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
202021
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
182012
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
172020
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
162020
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
122022
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
122021
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
112012
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
102016
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
82017
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
82014
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
72020
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
72019
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
72013
Preliminary Experimental Study on Closed-loop Flow Separation Control Utilizing Deep Q-Network over Fixed Angle-of-Attack Airfoil
S Shimomura, S Sekimoto, H Fukumoto, A Oyama, K Fujii, H Nishida
2018 Flow Control Conference, 3522, 2018
62018
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
62017
Flow control mechanism of a DBD plasma actuator for airfoils in low speed free-stream
S Sekimoto
Ph. D dissertation, University of Tokyo, 2015
62015
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
52018
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