Matsuno Takashi

Affiliation and department：

Research field (1)： Aerospace engineering

Research theme for competitive and other funds (10)：

2022 - 2025 Crossflow Reduction of Swept-Wing Boundary Layer and Delaying Turbulent Transition by Distributed Plasma Actuators
2020 - 2025 Control of Boundary-Layer Transition for Skin Friction Drag Reduction of Aircraft by Plasma Actuator
2021 - 2024 Detailed Evaluation and Flow Structure Optimization for Applicable Knowledge Acquisition of Low-Speed/ High- Angle-of-Attack Aerodynamics of a Forward Swept Wing
2020 - 2023 表面電荷制御による革新的流体制御技術の確立
2015 - 2018 Improvement of Multi-Electrode Plasma Actuator with Optimization of Discharge Parameters

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Papers (34)：

Satoshi SEKIMOTO, Kozo Fujii, Masayuki Anyoji, Yuma Miyakawa, Shinichiro Ito, Satoshi Shimomura, Hiroyuki Nishida, Taku Nonomura, Takashi Matsuno. Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number. Actuators. 2023. 12. 1
Asami HATAMOTO, Daichi HASEGAWA, Kumi NAKAI, Hiroyuki NISHIDA, Takashi MATSUNO. Experimental Study on Performance Characteristics of Plasma Actuator Composed of DC and AC Electrode. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 2020. 18. 6. 417-421
Kumi NAKAI, Hiroyuki NISHIDA, Norio ASAUMI, Yuhi TANAKA, Takashi MATSUNO. Development of Engineering Model Providing Body Force Distribution of Tri-Electrode Plasma Actuator. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2019. 62. 5. 247-255
Takashi MATSUNO, Ai FUKUDA, Hiromitsu KAWAZOE, Kumi NAKAI, Hiroyuki NISHIDA. The Effect of Voltage Frequency on Thrust Production of Multi-Electrode Plasma Actuator. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 2018. 16. 7. 582-587
松野隆, 菅原正隆, 橘一輝, 川添博光, 淺海典男, 松野伸介, 山口方士. Multi-Electrode Plasma Actuator for Flow Separation Control of Small-Scale Wing. 日本ガスタービン学会誌. 2017. 45. 6. 486-496

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MISC (61)：

瀬川武彦, 深潟康二, 松野隆, 野々村拓, 大西直文. プラズマアクチュエータ研究会 ~5年間の活動と今後の展望~. 日本機械学会流体工学部門ニューズレター「流れ」. 2019. 2019. 2. 3
Influence of Chordwise Location on the Aerodynamic Performance of Fins Vertically Mounted over the Wing. 2016. 47. 7p
NONOMURA Taku, SEGAWA Takehiko, FUKAGATA Koji, MATSUNO Takashi, SHIMIZU Kazuo, SHIRAISHI Hiroyuki. Summary. プラズマ・核融合学会誌. 2015. 91. 10. 671-673
MATSUNO Takashi, HONAMI Shinji, FUJII Kozo, SEKIMOTO Satoshi, IIDA Akiyoshi. Flow Measurement Technique. プラズマ・核融合学会誌. 2015. 91. 10. 661-664
FUKAGATA Koji, AONO Hikaru, FUJII Kozo, YAMADA Shunsuke, ISHIKAWA Hitoshi, MATSUNO Takashi. Experimental and Numerical Studies for Fundamental Flow Fields. プラズマ・核融合学会誌. 2015. 91. 10. 657-660

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Lectures and oral presentations (112)：

Optimization of Aerodynamic Control Performances of Plasma Actuator for Two Dimensional Wing Using EGO with Multi Additional Sampling
(流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM) 2018)
Study on Thrust Requirement for Plasma Actuator to Improve Flow around Airfoil
(日本ガスタービン学会定期講演会講演論文集 2017)
Influence of AC Voltage Waveform on Induced Jet from Multi - Electrode Plasma Actuator
(The Proceedings of Mechanical Engineering Congress, Japan 2017)
Optimization of Separation Control Performances of Plasma Actuator by EGO with Multi Additional Sampling
(The Proceedings of Mechanical Engineering Congress, Japan 2017)
Thrust Characteristics of High-Voltage Multi-Electrode Plasma Actuators
(飛行機シンポジウム講演集(CD-ROM) 2017)

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