Rchr
J-GLOBAL ID:201701019015062030   Update date: Nov. 07, 2024

Nonomura Taku

ノノムラ タク | Nonomura Taku
Affiliation and department:
Job title: Professor
Homepage URL  (1): http://www.fdl.mae.nagoya-u.ac.jp
Research field  (1): Aerospace engineering
Research keywords  (5): Reduced Order Medeling ,  Aeroacoustics ,  Flow Control ,  Experimental Aerodynamics ,  Fluid Dynamics
Research theme for competitive and other funds  (23):
  • 2022 - 2027 Machine Learning for Prediction and Control of Complex Dynamics Based on Integration of Mathematical and Data-Driven Methods
  • 2022 - 2025 分散データリザレクション:柔軟性と効率性を兼ね備えた計測情報再構成技術の創出
  • 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
Show all
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
more...
MISC (178):
  • 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
more...
Patents (1):
  • 流れ制御方法及び回転翼ユニット
Lectures and oral presentations  (62):
  • 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)
more...
Education (2):
  • - 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
Show all
Awards (19):
  • 2023/07 - 日本機械学会流体工学部門 一般表彰(貢献表彰) PA研究会主査;幹事
  • 2023/04 - NASA NASA Group Achievement Award
  • 2022/11 - 日本航空宇宙学会/航空宇宙数値シミュレーション技術シンポジウム 最優秀賞 流体力学部門 圧縮性低レイノルズ数流れにおける平板上の層流剥離泡および乱流遷移に対するマッハ数効果の数値的研究
  • 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)
  • 2022/08 - 一般社団法人 可視化情報学会 可視化情報学会 第33期 学会賞 論文賞 非定常せん断応力の可視化計測にむけた蛍光油膜法の開発
Show all
Association Membership(s) (6):
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
※ Researcher’s information displayed in J-GLOBAL is based on the information registered in researchmap. For details, see here.

Return to Previous Page