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WATANUKI Tadaharu  綿貫 忠晴

ORCIDConnect your ORCID iD *help
Researcher Number 00182965
Other IDs
Affiliation (based on the past Project Information) *help 1996 – 2002: University of Tokyo, Department of Aeronautics and Astronautics, Research Assist, 大学院・工学系研究科, 助手
1995 – 1996: 東京大学, 工学系研究科, 助手
1993 – 1994: 東京大学, 工学部, 助手
1986 – 1989: Department of Aeronautics, Faculty of Engineering, University of Tokyo, 工学部, 助手
Review Section/Research Field
Except Principal Investigator
Aerospace engineering / Aerospace engineering
Keywords
Except Principal Investigator
Computational Fluid Dynamics / 数値流体力学 / Supersonic aircraft / 超音速輸送機 / 超音速航空機 / Numerical Gas Dynamic Laser / Laser Power / Small-Signal Gain / Gas Dynamic Laser / 計算機プログラム … More / 燃焼 / 超音速流 / 数値計算コード / 振動緩和 / レーザー出力 / レーザー特性 / ガスダイナミックレーザー / 数値ガスダイナミックレ-ザ- / レ-ザ-出力 / 微小信号利得 / ガスダイナミックレ-ザ- / Navier-Stokes equation / Flow visualization / Wind tunnel testing / Vortex; Separated flow / Flow around high-angle-of-attack body / Slender body / 数値シミュレーション / ナヴィエ・ストークス方程式 / 流れの可視化 / 風洞試験 / 剥離流 / 渦 / 大迎角流れ / 細長物体 / Atmospheric model / Environmental adaptability / Ozone concentration prediction / Infra-red spectrometry / nitric oxides chemical reaction / Ozone / 大気モデル / 環境適合性 / オゾン濃度予測 / 赤外分光測定 / 窒素酸化物反応 / オゾン / Impinging Jet / Ground Effect / Jet / Nozzle Flow / Vertical Landing / Vertical Take-off and Landing Rocket / Reusable Space Transportaiton System / 再使用宇宙輸送システム / 空力特性 / 感圧塗料 / プラグノズル / 衝突噴流 / 地面効果 / 噴流 / ノズル流 / 垂直着陸 / 垂直離着陸ロケット / 再使用型宇宙輸送システム / Laminar flow control / Luminescent paint / Laser light interaction / Silicon oil film / Non-oscuring measurement / Skin friction drag / Surface skin friction / 測定法 / 境界層遷移 / 翼形 / 平板 / レーザー / 蛍光塗料 / 層流制御 / 発光性塗料 / レーザー光干渉 / シリコンオイル膜 / 非接触測定法 / 摩擦抵抗 / 表面摩擦 / Shock Tube / Shock Wave / Gas-Liquid Two-Phase Flow / Supersonic Transport / 衝撃波管実験 / 海洋環境 / 衝撃波管 / 衝撃波 / 気液二相流 / Engine noise / Airport noise / Nitric oxygen / Storatosphere / Ozone layr / Low sonic-boom design / Sonic-boom / 対流圏 / ナビエストークス方程式 / アロ-(矢形)翼 / 窒素化合物 / 矢形翼 / デルタ翼 / 環境課題 / エンジン騒音 / 空港騒音 / 窒素酸化物 / 成層圏 / オゾン層 / 低ブーム設計法 / ソニックブーム Less
  • Research Projects

    (7 results)
  • Co-Researchers

    (3 People)
  •  Prediction of Ozone Depletion in Upper Atmosphere by Nitric-Oxides in Supersonic Aircraft Engine Exhaust

    • Principal Investigator
      HIROTOSHI Kubota
    • Project Period (FY)
      2001 – 2002
    • Research Category
      Grant-in-Aid for Scientific Research (B)
    • Research Field
      Aerospace engineering
    • Research Institution
      The University of Tokyo
  •  Studies on Aerodynamic Characteristics of Next Generation's Vertical Take-off and Landing Reusable Rocket in Relation to Safety at Landing

    • Principal Investigator
      SUZUKI Kojiro
    • Project Period (FY)
      1999 – 2001
    • Research Category
      Grant-in-Aid for Scientific Research (B)
    • Research Field
      Aerospace engineering
    • Research Institution
      The University of Tokyo
  •  Non-osculating Surface Skin Friction Measurement Method with Use of Laser

    • Principal Investigator
      KUBOTA Hirotoshi
    • Project Period (FY)
      1997 – 1999
    • Research Category
      Grant-in-Aid for Scientific Research (B)
    • Research Field
      Aerospace engineering
    • Research Institution
      The University of Tokyo
  •  Study on Fluid Dynamic Effect of Supersonic Flight over the Ocean on Undersea Environment

    • Principal Investigator
      SUZUKI Kojiro
    • Project Period (FY)
      1996 – 1998
    • Research Category
      Grant-in-Aid for Scientific Research (C)
    • Research Field
      Aerospace engineering
    • Research Institution
      The University of Tokyo
  •  Study on Environmental issues at Flight of Supersonic Aircraft

    • Principal Investigator
      KUBOTA Hiroshi
    • Project Period (FY)
      1993 – 1996
    • Research Category
      Grant-in-Aid for Scientific Research (A)
    • Research Field
      Aerospace engineering
    • Research Institution
      UNIVERSITY OF TOKYO
  •  Studies on Numerical Gas Dynamic Laser Facility

    • Principal Investigator
      KUBOTA Hirotoshi
    • Project Period (FY)
      1987 – 1989
    • Research Category
      Grant-in-Aid for General Scientific Research (B)
    • Research Field
      Aerospace engineering
    • Research Institution
      The University of Tokyo
  •  Investigations for Flow Around slender bodies at high angles of attack

    • Principal Investigator
      KUBOTA Hirotoshi
    • Project Period (FY)
      1985 – 1986
    • Research Category
      Grant-in-Aid for General Scientific Research (B)
    • Research Field
      Aerospace engineering
    • Research Institution
      University of Tokyo
  • 1.  KUBOTA Hiroshi (30114466)
    # of Collaborated Projects: 5 results
    # of Collaborated Products: 0 results
  • 2.  SUZUKI Kojiro (10226508)
    # of Collaborated Projects: 2 results
    # of Collaborated Products: 0 results
  • 3.  MATSUZAKA Masayoshi (00010900)
    # of Collaborated Projects: 2 results
    # of Collaborated Products: 0 results

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