Rchr
J-GLOBAL ID:201501019409041786   Update date: Jan. 31, 2024

Kanazaki Masahiro

カナザキ マサヒロ | Kanazaki Masahiro
Affiliation and department:
Job title: 教授
Other affiliations (1):
Homepage URL  (1): https://kaken.nii.ac.jp/d/r/10392838.ja.html
Research field  (2): Aerospace engineering ,  Intelligent informatics
Research keywords  (5): デジタルフライト ,  時系列分析 ,  近似モデル ,  航空宇宙流体力学 ,  環境適合技術
Research theme for competitive and other funds  (8):
  • 2022 - 2025 Crossflow Reduction of Swept-Wing Boundary Layer and Delaying Turbulent Transition by Distributed Plasma Actuators
  • 2021 - 2024 Detailed Evaluation and Flow Structure Optimization for Applicable Knowledge Acquisition of Low-Speed/ High- Angle-of-Attack Aerodynamics of a Forward Swept Wing
  • 2016 - 2020 Time series aerodynamic control optimization for landing approach for supersonic aircraft subjected to unexpected turbulence
  • 2015 - 2018 Improvement of Multi-Electrode Plasma Actuator with Optimization of Discharge Parameters
  • 2014 - 2016 Investigation on Aerodynamic Performance of Vertical Aileron
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Papers (98):
  • Masahiro Kanazaki, Nao Setoguchi. Characteristics of Vortices around Forward Swept Wing at Low Speeds/High Angles of Attack. Aerospace. 2023
  • Yuki Kishi, Risato Yashiro, Masahiro Kanazaki. Low-Boom Design for Supersonic Transport with Canard and Forward-Swept Wings Using Equivalent Area Design Method. Aerospace. 2023
  • Chiba, K, Kanazaki, M. Feedback-Circulating Desgin Space Exploration by Multi-Sampling Kriging Model: Exploitation for the Lift Rise by an Aircraft Flap with Yaw-Wise Rotation. Proceedings on International Conference on Intelligent Systems, Metaheuristics and Swarm Intelligence. 2023
  • Hitomi Kano, Tomohiro Harada, Yukiya Miura, Masahiro Kanazaki. Hybrid Rocket Engine Design Using Pairwise Ranking Surrogate-assisted Differential Evolution. GECCO Companion. 2023. 1956-1962
  • Masahiro Kanazaki, Nao Setoguchi, Ryouta Saisyo. Evolutionary algorithm applied to time-series landing flight path and control optimization of supersonic transport. Neural Computing and Applications. 2023
more...
MISC (69):
  • 岸, 祐希, 金崎, 雅博, 杉浦, 正彦, 田辺, 安忠, 大山, 聖, 佐藤, 允, KISHI, Yuki, KANAZAKI, Masahiro, SUGIURA, Masahiko, TANABE, Yasutada, et al. 移動重合格子ソルバを用いた火星探査ヘキサコプタHAMILTONのロータ周りの空力特性調査-Numerical Investigation of Aerodynamic Characteristics around Hexacopter HAMILTON for Martian Exploration Using Moving Overlapped Grid. 宇宙航空研究開発機構特別資料: 第53回流体力学講演会/第39回航空宇宙数値シミュレーション技術シンポジウム論文集 = JAXA Special Publication: Proceedings of the 53rd Fluid Dynamics Conference / the 39th Aerospace Numerical Simulation Symposium. 2022. JAXA-SP-21-008. 149-155
  • Yuki Kishi, Masahiro Kanazaki, Masahiko Sugiura, Yasutada Tanabe, Akira Oyama, Makoto Sato. Numerical Analysis on Hovering Performance of Hexacopter “HAMILTON” for Mars Exploration. AIAA AVIATION 2022 Forum. 2022
  • Masahiko Sugiura, Yasutada Tanabe, Hideaki Sugawara, Keita Kimura, Akira Oyama, Makoto Sato, Kota Yoshikawa, Yuta Buto, Masahiro Kanazaki, Yuki Kishi, et al. Blade Shape Optimization of Mars Helicopter Exploring Pit Craters. 78th Vertical Flight Society Annual Forum and Technology Display, FORUM 2022. 2022
  • 杉浦, 正彦, 田辺, 安忠, 菅原, 瑛明, 木村, 桂大, 竹川, 国之, 大山, 聖, 佐藤, 允, 金崎, 雅博, 岸, 祐希, SUGIURA, Masahiko, et al. 火星ヘリコプタ用ロータブレード平面形状の空力的最適設計-Aerodynamic Optimal Design of Mars Helicopter Rotor Blade Planform. 宇宙航空研究開発機構特別資料: 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2020オンライン論文集 = JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online. 2021. JAXA-SP-20-008. 157-164
  • 大山 聖, 永井 大樹, 藤田 昂志, 安養寺 正之, 岡本 正人, 金崎 雅博, 高野 敦, 竹内 伸介, 安部 明雄, 佐々 修一, et al. 第2回火星飛行機高高度飛行試験(MABE2)の準備状況(その2). 大気球シンポジウム: 2020年度 = Balloon Symposium: 2020. 2020
more...
Lectures and oral presentations  (2):
  • 1405 Design Exploration of Airfoil for Mars Airplane
    (設計工学・システム部門講演会講演論文集 2010)
  • 2419 Application of Data Mining to Next Generation Aircraft's Wing
    (設計工学・システム部門講演会講演論文集 2009)
Works (3):
  • NAL小型超音速実験機の性能評価
    2001 -
  • 自動車エンジンサイクルシミュレーションと排気系形状の最適化
    2000 -
  • Design optimization of Exhaust Manifold for a Car Engine Using MOGA
    2000 -
Education (2):
  • - 2001 Tohoku University Graduate School, Division of Engineering
  • - 2001 Tohoku University
Professional career (1):
  • 博士 (東北大学)
Work history (4):
  • 2020/04 - 現在 Tokyo Metropolitan University
  • 2017/04 - 現在 Japan Aerospace Exploration Agency
  • 2012/04 - 2020/03 Tokyo Metropolitan University
  • 2004/04 - 2008/03 Japan Aerospace Exploration Agency Invited resercher
Awards (7):
  • 2018/08 - 日本航空宇宙学会・宇宙航空研究開発機構 最優秀賞(航空宇宙数値シミュレーション技術部門) 大規模非定常データに対する特徴構造抽出法の開発と大気突入カプセル後流解析への適用
  • 2017/06 - The American Institute of Aeronautics and Astronautics AIAA Honorable @Mentions: Exhibition hall contest on Instagram
  • 2016/04 - American Society of Civil Engineers 2015 Outstanding Reviewers
  • 2014/12 - The Japan Society for Evolutionary Computation JPNSEC2014 Best Paper Award in EC Workshop
  • 2012/11 - TOKYO DESIGN WEEK Co. Ltd. Tokyo Designers Week2012 Design Next Award Grand Prix
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Association Membership(s) (4):
進化計算学会 ,  American Institute of Aeronautics and Astronautics ,  The Japan Society for Aeronautical and Space Sciences ,  日本機械学会
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