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2020 Fiscal Year Annual Research Report

非定常3次元渦流れの計測融合シミュレーション法の開発

Research Project

Project/Area Number 18H03809
Research InstitutionTohoku University

Principal Investigator

大林 茂  東北大学, 流体科学研究所, 教授 (80183028)

Co-Investigator(Kenkyū-buntansha) 三坂 孝志  国立研究開発法人産業技術総合研究所, エレクトロニクス・製造領域, 研究部門付 (20645139)
浅井 圭介  東北大学, 工学研究科, 教授 (40358669)
野々村 拓  東北大学, 工学研究科, 准教授 (60547967)
奥泉 寛之  東北大学, 流体科学研究所, 技術専門職員 (60647957)
永井 大樹  東北大学, 流体科学研究所, 教授 (70360724)
Project Period (FY) 2018-04-01 – 2021-03-31
Keywords風洞 / 磁力支持 / 天秤 / データ同化 / 非定常3次元渦流れ
Outline of Annual Research Achievements

今年度は,風洞試験では,昨年度まで円柱を代表とする軸対称物体に対して行っていた磁力支持天秤装置(MSBS)実験法を,非軸対称物体に拡張するために,細長比L/H = 2.0 の3 次元正方角柱を対象に1-m 磁力支持天秤装置における3 次元角柱の位置計測手法を開発し,空力係数及び背圧係数の計測を行い,さらに油膜法による模型表面の流れ場の可視化を行い,再付着流れが空力特性に及ぼす影響を解明した.
新たに提案した位置計測手法により角柱模型を対象に各軸±5 mm deg の範囲で誤差0.1mm degの精度で位置計測が可能になった.縦3 分力の変動ではSt = 0.03 付近にピークが存在した.迎角が増加することにより,模型側面の剥離せん断層が再付着せず,揚力係数およびモーメント係数の勾配が緩やかになった.背圧係数にはレイノルズ依存性が見られ,レイノルズ数が減少することで背圧係数が低下した.また,蛍光油膜による可視化から.迎角が増加することで模型上面の再付着位置が下流に移動し,迎角4 deg の時に再付着が無くなり剥離することが分かった.
また,数値流体解析では,気流に平行に支持された低細長比円柱が振動した際の流れ構造を詳細に調査し,空気力と流れ構造の関連性を明らかにした.計算結果より得られた空気力について,静止時は風洞実験結果とよく一致した.円柱を加振した際は,k = 0.10 でピークを持つようにCx が増加し,Cx の標準偏差も同時に増加した.時間平均した流れ場を見ると,主流方向速度において,静止時は軸対称性があるのに対し,加振時は軸対称性が失われた.位相平均を行うと,位相が進むにつれて,流れ構造が形状を保ったまま流れ後方に移流することが分かった.POD を用いた流れ場解析では,静止時のモードはらせん構造が卓越していた.k = 0.10 で加振した時のモードはある平面に対して反対称なフラッピング構造が卓越していた.

Research Progress Status

令和2年度が最終年度であるため、記入しない。

Strategy for Future Research Activity

令和2年度が最終年度であるため、記入しない。

  • Research Products

    (18 results)

All 2021 2020

All Journal Article (12 results) (of which Int'l Joint Research: 6 results,  Peer Reviewed: 12 results,  Open Access: 11 results) Presentation (6 results) (of which Int'l Joint Research: 6 results)

  • [Journal Article] Low-Reynolds-Number Flowfield of Wing with Control Surface in Propeller Slipstream2021

    • Author(s)
      Ikami Tsubasa、Fujita Koji、Nagai Hiroki
    • Journal Title

      Journal of Aircraft

      Volume: 58 Pages: 228~235

    • DOI

      10.2514/1.C035880

    • Peer Reviewed / Open Access
  • [Journal Article] Sub-millimeter resolution pressure measurement on free flight model at Mach 1.5 using novel non-intrusive optical technique2021

    • Author(s)
      Kurihara Daiki、Gonzales Joseph P.、Claucherty Steven L.、Kiritani Hideki、Fujita Koji、Jemcov Aleksandar、Nagai Hiroki、Sakaue Hirotaka
    • Journal Title

      Experimental Thermal and Fluid Science

      Volume: 120 Pages: 110243~110243

    • DOI

      10.1016/j.expthermflusci.2020.110243

    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Journal Article] Effects of Propeller Position and Rotation Direction on the Ishii Wing at a Low Reynolds Number2021

    • Author(s)
      FUJITA Koji、KURANE Kakeru、TAKAHASHI Koichi、NAGAI Hiroki
    • Journal Title

      TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

      Volume: 64 Pages: 22~30

    • DOI

      10.2322/tjsass.64.22

    • Peer Reviewed / Open Access
  • [Journal Article] Shape optimization for suppressing coherent structure of two-dimensional open cavity flow2021

    • Author(s)
      NAKAZAWA Takashi、MISAKA Takashi、POIGNARD Clair
    • Journal Title

      Journal of Fluid Science and Technology

      Volume: 16 Pages: 0002~0002

    • DOI

      10.1299/jfst.2021jfst0002

    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Journal Article] Analysis of unsteady flow around an axial circular cylinder of critical geometry using combined synchronous measurement in magnetic suspension and balance system2021

    • Author(s)
      Yokota Sho、Ochiai Taku、Ozawa Yuta、Nonomura Taku、Asai Keisuke
    • Journal Title

      Experiments in Fluids

      Volume: 62 Pages: 1-20

    • DOI

      10.1007/s00348-020-03101-7

    • Peer Reviewed
  • [Journal Article] Application of pressure-sensitive paint for the characterization of mixing with various gases in T-type micromixers2020

    • Author(s)
      Huang Chih-Yung、Hu Yu-Hsiang、Wan Shaw-An、Nagai Hiroki
    • Journal Title

      International Journal of Heat and Mass Transfer

      Volume: 156 Pages: 119710~119710

    • DOI

      10.1016/j.ijheatmasstransfer.2020.119710

    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Journal Article] Ruthenium-based fast-responding pressure-sensitive paint for measuring small pressure fluctuation in low-speed flow field2020

    • Author(s)
      Egami Y、Hasegawa Y、Matsuda Y、Ikami T、Nagai H
    • Journal Title

      Measurement Science and Technology

      Volume: 32 Pages: 024003~024003

    • DOI

      10.1088/1361-6501/abb916

    • Peer Reviewed / Open Access
  • [Journal Article] Real-time estimation of airflow vector based on lidar observations for preview control2020

    • Author(s)
      Kikuchi Ryota、Misaka Takashi、Obayashi Shigeru、Inokuchi Hamaki
    • Journal Title

      Atmospheric Measurement Techniques

      Volume: 13 Pages: 6543~6558

    • DOI

      10.5194/amt-13-6543-2020

    • Peer Reviewed / Open Access
  • [Journal Article] Finite surface discretization for incompressible Navier-Stokes equations and coupled conservation laws2020

    • Author(s)
      Hokpunna Arpiruk、Misaka Takashi、Obayashi Shigeru、Wongwises Somchai、Manhart Michael
    • Journal Title

      Journal of Computational Physics

      Volume: 423 Pages: 109790~109790

    • DOI

      10.1016/j.jcp.2020.109790

    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Journal Article] Streamline pair selection for comparative flow field visualization2020

    • Author(s)
      Sawada Shoko、Itoh Takayuki、Misaka Takashi、Obayashi Shigeru、Czauderna Tobias、Stephens Kingsley
    • Journal Title

      Visual Computing for Industry, Biomedicine, and Art

      Volume: 3 Pages: 1-35

    • DOI

      10.1186/s42492-020-00056-8

    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Journal Article] Study on decay characteristics of vertical four-vortex system for increasing airport capacity2020

    • Author(s)
      Cho Junho、Lee Bok Jik、Misaka Takashi、Yee Kwanjung
    • Journal Title

      Aerospace Science and Technology

      Volume: 105 Pages: 106017~106017

    • DOI

      10.1016/j.ast.2020.106017

    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Journal Article] Aerodynamic Characteristics of Low-Fineness-Ratio Freestream-Aligned Cylinders with Magnetic Suspension and Balance System2020

    • Author(s)
      Shinji K.、Nagaike H.、Nonomura T.、Asai K.、Okuizumi H.、Konishi Y.、Sawada H.
    • Journal Title

      AIAA Journal

      Volume: 58 Pages: 3711~3714

    • DOI

      10.2514/1.J058925

    • Peer Reviewed / Open Access
  • [Presentation] Aerodynamic Measurements of Turbojav using 1-m Magnetic Suspension and Balance System2021

    • Author(s)
      Hiroyuki Okuizumi, Kasumi Sasaki, Yasufumi Konishi, Shigeru Obayashi
    • Organizer
      AIAA SciTech Forum and Exposition (Virtual Event)
    • Int'l Joint Research
  • [Presentation] A new position and attitude measurement method for complex shape models with non circular cross section in Magnetic Suspension and Balance System2021

    • Author(s)
      M. Horiguchi, Y. Saito, T. Nonomura, K. Asai, Y. Konishi, H. Okuizumi, H. Sawada, S. Obayashi
    • Organizer
      AIAA SciTech Forum and Exposition (Virtual Event)
    • Int'l Joint Research
  • [Presentation] Aerodynamic Characteristics of Circular Cylinders with Fineness Ratios Lower than 0.5 Measuredby a Magnetic Suspension and Balance System2020

    • Author(s)
      12.Y. Abe, S. Yokota, T. Nonomura, H. Sawada, A. Yakeno, K. Asai, S. Obayashi
    • Organizer
      The Seventeenth International Conference on Flow Dynamics, Online
    • Int'l Joint Research
  • [Presentation] Wind-tunnel Experiment of Square-Cylinder Model in 1.0-mMagnetic Suspension and Balance System2020

    • Author(s)
      13.M. Horiguchi, Y. Saito,T. Nonomura, K. Asai, Y. Konishi, H. Okuizumi, H. Sawada, S. Obayashi
    • Organizer
      The Seventeenth International Conference on Flow Dynamics, Online
    • Int'l Joint Research
  • [Presentation] Aerodynamic Characteristics of Circular Cylinders with Fineness Ratios Lower than 0.5 Measured by a Magnetic Suspension and Balance Sysytem2020

    • Author(s)
      M. Kuwata, Y. Abe, S. Yokota, T. Nonomura, H. Sawada, A. Yakeno, K. Asai, and S. Obayashi
    • Organizer
      The Seventeenth International Conference on Flow Dynamics, Online
    • Int'l Joint Research
  • [Presentation] Investigation on Near-wake Structure of Magnetically Levitated Freestream-aligned Circular Cylinder with Finenss Ratio 0.5 - 2.0 in 0.3-m MSBS2020

    • Author(s)
      S. Yokota, Y. Saito, T. Nonomura, and K. Asai
    • Organizer
      The Seventeenth International Conference on Flow Dynamics, Online
    • Int'l Joint Research

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Published: 2021-12-27  

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