Nagoya University, Tokai National Higher Education and Research System Fluid Dynamic Labratory, Department of Aerospace Engineering, Graduate School of Engineering
About Nagoya University, Tokai National Higher Education and Research System Fluid Dynamic Labratory, Department of Aerospace Engineering, Graduate School of Engineering
2022 - 2025 Insect flight mechanisms in high flight attitude
2021 - 2025 データ同化による風洞実験デジタルツイン
2020 - 2023 表面電荷制御による革新的流体制御技術の確立
2020 - 2023 Data-driven-science-based spatio-temporal super-resolution measurement of a large scale turbulent structure of supersonic jet
2019 - 2022 Next-generation flow control using the reduced-order model based on advanced unsteady flow measurement
2019 - 2022 Measurement of unsteady flow generated by deformable object for understanding locomotion principle
2018 - 2021 Development of measurement fusion simulation method for unsteady three-dimensional vortex flow
2018 - 2020 Drag force and flow field measurement of a sphere in the low Reynolds number and high Mach number flows using magnetic suspension and balance system
2017 - 2020 Construction of prediction model of multiple supersonic jets based on Advanced Measurement and High Resolution Numerical Simulations
2017 - 2020 Examination on Turbulence Mixing and Sound Generation Phenomena in High Mach Number Multiphase Flows by DNS Analysis
2019 - 2020 Spatio-temporal super-resolution measurement of a supersonic jet using a low-dimensional model and clarification of acoustic wave generation mechanism
2016 - 2018 Development of numerical method for thermos-fluid analysis around moving objects in multi-phase flow
2015 - 2018 Analysis of Flow Control Authority of DBD Plasma Actuator in Practical Use
2015 - 2017 Establishment of Technique for Fast High-order-accurate Unstructured-mesh Fluid Solver on Exa-scale Computer
2013 - 2017 Characterization of Generation Mechanism of Nonlinear Acoustic Waves from Supersonic Jet and Quantitative Prediction of Acoustic Waves
2012 - 2015 Key technology Research and High-altitude demonstration to realize the world first Mars exploration using Airplane
2012 - 2015 Mechanism of plasma-actuator induced flows toward better control parameter settings
2012 - 2015 Construction of LES Model based on DNS Analysis of High Mach Number Multiphase Flow
2011 - 2013 Clarification of nonlinear aeroacoustic waves from a supersonic jet impinging on objects with data-mining
2008 - 2010 Research on plasma actuator flow control that pays attention to localization flow
2007 - 2008 ロケット打ち上げ時に発生する非線形空力音に関する研究
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Papers (223):
Di Kong, Eihiro Li, Kazuki Uchida, Takayuki Nagata, Taku Nonomura. Measuring tiny pressure fluctuations using fast pressure-sensitive paint and phase-lock technology: Uniformity evaluation of resonance tube. Measurement. 2025
Yuto Iwasaki, Yasuo Sasaki, Takayuki Nagata, Sayumi Kaneko, Taku Nonomura. Dynamic mode decomposition based on expectation-maximization algorithm for simultaneous system identification and denoising. Mechanical Systems and Signal Processing. 2025
Rodrigo Viguera, Yasuo Sasaki, Taku Nonomura. Experimental Analysis of Flow Separation Control by a Dielectric Barrier Discharge Plasma Actuator in Burst-in-Burst Actuation Mode. Actuators. 2024
Chungil Lee, Yuta Ozawa, Takayuki Nagata, Tim Colonius, Taku Nonomura. Superresolution and analysis of three-dimensional velocity fields of underexpanded jets in different screech modes. Physical Review Fluids. 2024
Akitoshi Matsui, Chiaki Kawase, Yosuke Sugioka, Keisuke Asai, Taku Nonomura. Measurement of pressure fluctuation distribution on a flat wall behind supported square cylinder with pressure-sensitive paint. Experimental Thermal and Fluid Science. 2024. 157
佐藤 允, 岡田 浩一, 浅田 健吾, 青野 光, 野々村 拓, 藤井 孝藏. 広範なレイノルズ数におけるプラズマアクチュエータを用いた翼周り剥離制御の統一的なメカニズム : 論文賞受賞記念解説-Unified Mechanisms for Separation Control around Airfoil using Plasma Actuator with Burst Actuation over Reynolds Number Range of 103-106. ながれ : 日本流体力学会誌 = Nagare : journal of Japan Society of Fluid Mechanics. 2022. 41. 3. 151-155
大林茂, 野本京佑, 焼野藍子, 野々村拓. An Attempt to Construct a Digital Twin of Wind Tunnel Experiments by Data Assimilation. 飛行機シンポジウム講演集(CD-ROM). 2022. 60th
岡慶典, 永田貴之, 小澤雄太, 野々村拓, 浅井圭介. Characteristics Evaluation of Free-base Porphyrins Anodized-Aluminum Pressure-Sensitive Paint by Visualizing of Normal Shock Wave and Application to the Supersonic Cavity Flow Measurement. 衝撃波シンポジウム講演論文集(CD-ROM). 2022. 2021
永田貴之, 高橋俊, 水野祐介, 野々村拓. Analysis of Particle Mach Number and Relative Position Effects on the Aerodynamic Interference between Two Particles by Direct Numerical Simulation. 衝撃波シンポジウム講演論文集(CD-ROM). 2022. 2021
永田貴之, 野々村拓. Numerical Study of Mach Number Effects on Laminar Separation Bubble and Turbulent Transition on a flat Plate under Compressible Low Reynolds Number flows. 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). 2022. 54th-40th
Effect of Angle of Attack on Aerodynamic Characteristics of Freestream-Aligned Circular Cylinder with Fineness Ratio of 1.0
(AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 2022)
Investigation of maximum velocity induced by body-force fields for simpler modeling of plasma actuators
(AIAA Aerospace Sciences Meeting, 2018 2018)
Direct numerical simulation of flow past a sphere at a reynolds number between 500 and 1000 in compressible flows
(AIAA Aerospace Sciences Meeting, 2018 2018)
Evaluation of discharge energy for separation flow control around NACA0015 airfoil controlled by nanosecond-pulse-driven plasma actuator
(AIAA Aerospace Sciences Meeting, 2018 2018)
Large-eddy simulations of flow control effects of a DBD plasma actuator at various burst frequencies on a dynamic flowfield around a pitching NACA0012 airfoil at reynolds number of 256,000
(AIAA Aerospace Sciences Meeting, 2018 2018)
- 2008 The University of Tokyo Graduate School, Division of Engineering Department of Aeronautics and Astronautics
- 2003 Nagoya University Faculty of Engineering Mechanical and Aerospace Engineering
Professional career (1):
Ph. D (Engineering) (Department of Aeronautics and Astronautics) (The University of Tokyo)
Work history (5):
2023/11 - 現在 Nagoya University, Tokai National Higher Education and Research System Department of Aerospace Engineering, Graduate School of Engineering Professor
2016/08 - 2023/10 Tohoku University Graduate School of Engineering Associate Professor
2011/04 - 2016/07 Japan Aerospace Exploration Agency Associate Professor
2009/04 - 2011/03 Japan Aerospace Exploration Agency Project Researcher
2008/04 - 2009/03 Japan Aerospace Exploration Agency JSPS Research fellow
Committee career (9):
2021/04 - 現在 日本航空宇宙学会 論文編集委員会
2020/04 - 現在 日本機械学会 宇宙工学部門委員
2020/03 - 現在 可視化情報学会 可視化情報学会誌編集委員
2020/03 - 現在 American Institute of Aeronautics and Astronautics Fluid Dynamic Technical Committee
2017/05 - 現在 日本流体力学会 ながれ編集委員
2024/04 - 2026/03 Japan Society of Fluid Mechanics Director
2023/05 - 2025/03 Editorial board of Transaction of Japan Society of Aeronautics and Space Science Editor in Cheif
2022/09 - 日本流体力学会 日本流体力学会論文賞 Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 103 -106, Physics of Fluids, Vol. 32, 025102 (2020)
2022/01 - American Institute of Aeronautics and Astromautics Associate Fellow AIAA
2021/11 - 日本機械学会流体工学部門 日本機械学会流体工学部門 一般表彰 フロンティア表彰
2021/09 - 日本機械学会計算力学部門 日本機械学会部門計算力学部門 部門賞 業績賞
2020/09 - Encouragement Award Denoising the Pressure Sensitive Paint Measurement of Unsteady Low-Speed Flow using Extended Kalman Filter Based Dynamic Mode Decompisition
2020/04 - Tohoku University Distinguished Researcher
2020/04 - Editorial board of Fluid Dynamics Research Outstanding Reviewer award of Fluid Dynamic Research
2019/09 - Japan Society of Fluid Mechanics Award for Distinguished Young Researcher in Fluid Mechanics Research on High-order Weighted Schemes for Aeroacoustic Analysis of High Seed Flow
2019/04 - Ministry of Education, Science Sports and Culture and the Science and Technology Agency Prize of Young Researcher Research on Prediction of Aeroacoustic Waves from Supersonic Jet by Highly Accurate Numerical Simulation
2018/06 - American Institute of Aeronautics and Astronautics AIAA 2018 Aerodynamics Measurement Technology (AMT) Best Paper. First Results of Lifetime-Based Unsteady PSP Measurement on a Pitching Airfoil in Transonic Flow
The Society of Insturment and Control Endineers
, 可視化情報学会
, American Institute of Aeronautics and Astronautics
, THE JAPAN SOCIETY OF FLUID MECHANICS
, THE JAPAN SOCIETY OF MECHANICAL ENGINEERS
, Japan Society of Aeronautics and Space Science