横田 翔

(Sho Yokota)

博士後期課程 1 年

経歴

・2021.04-現在 日本学術振興会 特別研究員 DC1

・2021.04-現在 東北大学 学際高等研究教育院 博士研究教育院生(先端基礎科学)

・2021.04-現在 青葉工学振興会 令和 3 年度奨学生

・2020.04-2021.03 東北大学 学際高等研究教育院 修士研究教育院生(先端基礎科学)

・2019.04-2020.03 田中貴金属記念財団 2019 年度 奨学生

学歴

・2021.04-現在 東北大学大学院 工学研究科 航空宇宙工学専攻 博士後期課程

・2019.04-2021.03 東北大学大学院 工学研究科 航空宇宙工学専攻 博士前期課程

・2016.04-2019.03 東北大学 工学部 機械知能・航空工学科

受賞

・2021.03 2020 年度 日本機械学会 三浦賞 

・2020.12 The 17th International Conference on Flow Dynamics, Best Presentation Award for Young Researcher 

・2019.12 The 16th International Conference on Flow Dynamics, Best Presentation Award for Young Researcher 

・2018.04 東北大学工学部・工学研究科 グローバル工学奨励賞 2017

査読付き学術雑誌

2) Kuwata, M., Abe, Y., Yokota, S., Nonomura, T., Sawada, H., Yakeno, A., Asai, K., and Obayashi, S., Flow characteristics around extremely low fineness-ratio circular cylinders,” Physical Review Fluids, APS, vol. 6, No. 5, 2021 (Editors’ Suggestion)

1) Yokota, S., Ochiai, T., Ozawa, Y., Nonomura, T., and Asai, K., “Analysis of unsteady flow around an axial circular cylinder of critical geometry using combined synchronous measurement in magnetic suspension and balance system,” Experiments in Fluids, Springer, vol. 62, 1, 2021

国際会議における発表

10) Yokota, S., Hassan, M., Nonomura, T., and Asai, K., “Effect of Angle of Attack on Aerodynamic Characteristics of Freestream-Aligned Circular Cylinder with Fineness Ratio of 1.0,” AIAA SciTech 2022, California, USA, January, 2022 (Accepted)

9) Tashiro, K., Yokota, S., Zignov, F., Ozawa, Y., Nonomura, T., and Asai, K., “Aerodynamic Characteristics of the Slanted Cylinder Afterbody Investigated in 0.3-m Magnetic Suspension and Balance System,” 18th International Conference on Flow Dynamics, Miyagi, Japan, October, 2021

8) Inomata, C., Yokota, S., Nonomura, T., and Asai, K., “Magnetic Levitation of Reentry Capsule Towards Wind Tunnel Testing,” 18th International Conference on Flow Dynamics, Miyagi, Japan, October, 2021

7) Yokota, S., Nonomura, T., and Asai, K., “Effect of Angle of Attack on Freestream-Aligned Circular Cylinder with Fineness Ratio of 1.0 – Updateof Experimental Research in 0.3-m MSBS,” 18th International Conference on Flow Dynamics, Miyagi, Japan, October, 2021

6) Yokota, S., Saito, Y., Nonomura, T., and Asai, K., “Investigation on Near-wake Structure of Magnetically Levitated Freestream-aligned Circular Cylinder with Fineness Ratio 0.5 – 2.0 in 0.3-m MSBS,” 17th International Conference on Flow Dynamics, Miyagi, Japan, October, 2020

5) Kuwata, M., Abe, Y., Yokota, S., Nonomura, T., Sawada, H., Yakeno, A., Asai, K., and Obayashi, S., “Aerodynamic characteristics of circular cylinders with fineness ratios lower than 0.5 measured by a magnetic suspension and balance system,” 17th International Conference on Flow Dynamics, Miyagi, Japan, October, 2020

4) Kuwata, M., Yokota, S., Sawada, H., Abe, Y., Yakeno, A., Nonomura, T., Asai, K., and Obayashi, S., “Drag Coefficients of Circular Cylinders with Low Fineness Ratio less than 0.50 measured by 0.1 and 0.3 Magnetic Suspension and Balance Systems,” AIAA SciTech Forum 2020, Florida, USA, January, 2020

3) Yokota, S., Nonomura, T., and Asai, K., “Investigation of Characteristic Flow Structure around Circular Cylinders with Fineness Ratio 0.5 – 2.25 in 0.3-m MSBS,” 16th International Conference on Flow Dynamics, Miyagi, Japan, November, 2019

2) Hassan, M., Yokota, S., Nonomura, T., and Asai, K., “Effect of Angle of Attack of up to 15 Degree on Aerodynamic Force on a Freestream-aligned Circular Cylinder of Aspect Ratio 1.0 in 0.3-m Magnetic Suspension and Balance System,” 16th International Conference on Flow Dynamics, Miyagi, Japan, November, 2019

1) Yokota, S., Ochiai, T., Ozawa, Y., Nonomura, T., and Asai, K., “Effect of Fineness Ratio of 0.5 – 2.0 on the Wake Structure around a Circular Cylinder Measured using Time-resolved PIV,” ASME-JSME-KSME Joint Fluids Engineering Conference 2019, AJKFLUIDS2019-5530, California, USA, July, 2019 

国内学会における発表

2) 横田翔,野々村拓,浅井圭介,”気流と平行に磁力支持された円柱の剥離せん断層の不安定性に関する研究,” 日本流体力学会 年会 2021,オンライン,9 月,2021 年

1) 横田翔,落合拓,安保巧,小澤雄太,野々村拓,浅井圭介,”磁力支持天秤装置を用いた細長比0.5の円柱周りの流れ場解析,” 日本航空宇宙学会北部支部 2019 年講演会,宮城,3 月,2019 年

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