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J-GLOBAL ID:201901011664706234
Update date: Sep. 06, 2024
Sato Shintaro
サトウ シンタロウ | Sato Shintaro
Affiliation and department:
Job title:
助教
Research field (3):
Fluid engineering
, Basic plasma science
, Aerospace engineering
Research theme for competitive and other funds (8):
- 2024 - 2029 航空機の空力設計を変革する革新的流体低次元モデルの幾何学的定式化
- 2024 - 2027 Drastic Acceleration of Fluid Simulation Using Combination of Low-Dimensional and High-Dimensional Models
- 2024 - 2027 電荷制御に基づく革新的イオン風生成技術によるエアロイオニクスの確立
- 2021 - 2025 アポステリオリ流体幾何学の創出
- 2021 - 2024 Establishment of active airflow control system based on unsteady aerodynamics
- 2020 - 2023 表面電荷制御による革新的流体制御技術の確立
- 2018 - 2020 無人航空機のロバスト化に向けたプラズマアクチュエータによる流れの時空間的能動制御
- 2019 - 誘電体表面電荷制御に基づく低電圧作動プラズマアクチュエータの開発-小型模型飛行機を用いた実証実験-
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Papers (25):
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Yuto Nakamura, Shintaro Sato, Naofumi Ohnishi. Application of proper orthogonal decomposition to flow fields around various geometries and reduced-order modeling. Computer Methods in Applied Mechanics and Engineering. 2024. 432. 117340-117340
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Yasuhito Okano, Shintaro Sato, Hiroki Nagai, Naofumi Ohnishi. Dynamic instability in lift-type reentry capsule at supersonic flow. Physics of Fluids. 2024. 36. 7
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Yuto Nakamura, Shintaro Sato, Naofumi Ohnishi. Proper orthogonal decomposition method of constructing a reduced-order model for solving partial differential equations with parametrized initial values. Partial Differential Equations in Applied Mathematics. 2024. 100654-100654
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Shintaro Sato, Mahoro Sakurai, Naofumi Ohnishi. Ionic wind generation through coplanar discharge: A plasma actuator without exposed electrodes. AIP Advances. 2023. 13. 6
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Hideto Tamura, Shintaro Sato, Naofumi Ohnishi. Numerical simulation of atmospheric-pressure surface dielectric barrier discharge on a curved dielectric with a curvilinear mesh. Journal of Physics D: Applied Physics. 2023. 56. 4. 045202-045202
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MISC (2):
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SATO Shintaro, OHNISHI Naofumi. S0530103 Numerical Analysis of Pulse Discharge Process in DBD Plasma Actuator. Mechanical Engineering Congress, Japan. 2015. 2015. "S0530103-1"-"S0530103-5"
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Theoretical analysis of pulse interval in DBD plasma actuator. 2015. 46. 5p
Education (3):
- 2017 - 2019 Tohoku University Graduate School of Engineering Department of Aerospace Engineering
- 2015 - 2017 Tohoku University Graduate School of Engineering Department of Aerospace Engineering
- 2011 - 2015 Tohoku University Faculty of Engineering Department of Mechanical and Aerospace Engineering
Professional career (1):
Work history (2):
- 2019/10 - 現在 Tohoku University Graduate School of Engineering, Department of Aerospace Engineering
- 2018/04 - 2019/09 日本学術振興会 特別研究員(DC2)
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