Ito Takeshi

イトウタケシ | Ito Takeshi

Affiliation and department：
Job title： Senior Chief Officer of Aviation Innovation

Research field (1)： Aerospace engineering

Research keywords (20)：プラズマトロン , アーク加熱風洞 , 境界層遷移、ルードビークチューブ , プラズマ電子密度 , ハイフレックス , インレット , 極超音速 , ソニックブーム , 消防飛行艇 , 音源探査 , 低速風洞 , Plasmatron , Arc-heated wind tunnel , Ludwieg Tube , Boundary Layer Transition , Plasma Electra Density , HYFLEX , Hypersonic , Aeroacousitc measurement , Low-speed wind tunnel

Research theme for competitive and other funds (2)：

風洞を用いた実験的空力研究
Aerodynamic Research using Wind tunnels

Papers (6)：

Hiroki Ura, Yuzuru Yokokawa, Taro Imamura, Takeshi Ito, Kazuomi Yamamoto. Airframe noise measurements by using a simplified high-lift model. 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 2010. 2. 1220-1230
Kazuhisa Fujita, Masahito Mizuno, Kiyomichi Ishida, Takeshi Ito. Spectroscopic Flow Evaluation in Inductively Coupled Plasma Wind Tunnel. JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER. 2008. 22. 4. 685-694
Hiroki Ura, Yuzuru Yokokawa, Taro Imamura, Takeshi Ito, Kazuomi Yamamoto. Investigation of airframe noise from high lift configuration model. 46th AIAA Aerospace Sciences Meeting and Exhibit. 2008
Masahiro Kanazak, Yuzuru Yokokawa, Mitsuhiro Murayama, Takeshi Ito, Shinkyu Jeong, Kazuomi Yamamoto. Nacelle chine installation based on wind-tunnel test using efficient global optimization. Transactions of the Japan Society for Aeronautical and Space Sciences. 2008. 51. 173. 146-150
Yuzuru Yokokawa, Hiroki Ura, Taro Imamura, Takeshi Ito, Kazuomi Yamamoto. Detail observation of noise and aerodynamics for high-lift configuration model in JAXA. Turkish Acoustical Society - 36th International Congress and Exhibition on Noise Control Engineering, INTER-NOISE 2007 ISTANBUL. 2007. 2. 743-753

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MISC (34)：

Takeshi ITO, Hiroki URA, Kazuyuki NAKAKITA, Yuzuru YOKOKAWA, Wing F. NG, Ricardo A. BURDISSO, Akihito IWASAKI, Toshimi FUJITA, Norihisa ANDO, Naoki Shimada, et al. Aerodynamic/Aeroacoustic testing in Anechoic Closed Test Sections of Low-speed Wind Tunnels. AIAA paper 2010-3750. 2010
Takeshi ITO, Hiroyuki KATO, Yushi GODA, Shinji TAGAWA, Eiichi NEGISHI. Water-Dropping Aerodynamics for Fire-Fighting Amphibian. Proceedings of ICAS 2010-2.11.1. 2010
Takeshi ITO, Hiroki URA, Kazuyuki NAKAKITA, Yuzuru YOKOKAWA, Wing F. NG, Ricardo A. BURDISSO, Akihito IWASAKI, Toshimi FUJITA, Norihisa ANDO, Naoki Shimada, et al. Aerodynamic/Aeroacoustic testing in Anechoic Closed Test Sections of Low-speed Wind Tunnels. AIAA paper 2010-3750. 2010
Takeshi ITO, Hiroyuki KATO, Yushi GODA, Shinji TAGAWA, Eiichi NEGISHI. Water-Dropping Aerodynamics for Fire-Fighting Amphibian. Proceedings of ICAS 2010-2.11.1. 2010
Takeshi ITO, Hiroki URA, Ken KAJITANI, Hiroyuki TANAKA. Aeroacoustic Noise Survey on Supersonic Transport Airframe in Large-scale Aerodynamic Low-speed Wind Tunnel. AIAA 2008-48. 2008

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Education (4)：

- 1989 Nagoya University
- 1989 Nagoya University Graduate School, Division of Engineering
- 1988 Nagoya University School of Engineering
- 1988 Nagoya University Faculty of Engineering

Professional career (1)：

Doctor of Engineering (Nagoya University)

Work history (22)：

2021/11 - 現在宇宙航空研究開発機構航空技術部門航空イノベーション統括
2015/04 - 現在 Nagoya University
2020/04 - 2021/10 Japan Aerospace Exploration Agency
2019/04 - 2020/03 宇宙航空研究開発機構航空技術部門次世代航空イノベーションハブ副ハブ長
2018/04 - 2019/03 宇宙航空研究開発機構航空技術部門次世代航空イノベーションハブ企画連携チームチーム長

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Committee career (16)：

2023/04 - 現在科学技術・学術審議会専門委員(技術士分科会)
2023/04 - 現在日本航空宇宙学会監事
2021/04 - 現在日本航空宇宙学会航空宇宙ビジョン委員会航空ビジョン小委員会委員長
2019/04 - 2021/03 日本航空宇宙学会監事
2009 - ~ :日本航空宇宙学会航空ビジョン委員会幹事

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Association Membership(s) (4)：

AIAA , 日本航空宇宙学会 , The Japan Society for Aeronautical and Space Science , American Institute of Aeronautics and Astronautics (AIAA)

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