Kanazaki Masahiro 金崎雅博

… Alternative Names

KANAZAKI Masahiro 金崎雅博

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Researcher Number	10392838
Other IDs
Affiliation (Current)	2025: 東京都立大学, システムデザイン研究科, 教授
Affiliation (based on the past Project Information) *help	2021 – 2024: 東京都立大学, システムデザイン研究科, 教授 2012 – 2019: 首都大学東京, システムデザイン研究科, 准教授 2015: 首都大学東京, 大学院システムデザイン研究科, 准教授
Review Section/Research Field	Principal Investigator Basic Section 24010:Aerospace engineering-related / Aerospace engineering / Intelligent informatics Except Principal Investigator Aerospace engineering / Basic Section 24010:Aerospace engineering-related / Fluid engineering
Keywords	Principal Investigator 数値流体力学 / 超音速旅客機 / 翅脈 / 生物模倣 / 火星飛行機 / 流れ構造の最適設計 / 超音速前進翼 / 低速高迎角 / 高揚力装置 / 体積力モデリング … More / 低速高迎角特性 / 前進翼 / 流体 / 航空宇宙工学 / 空力―飛行力学連成 / 着陸経路 / 離着陸 / 超音速航空機 / 飛行力学 / 進化計算 / 空力―飛行力学連成計算 / 空気力学 / 時系列分析 / 近似モデル / デジタルフライト / 時系列的データ / フライトシミュレーション / Numerical Approach / Time Series Analysis / Surrogate model / Fluid Dynamics / Flight Simulation … More Except Principal Investigator プラズマアクチュエータ / 最適設計 / 流体制御 / 風洞試験 / 数値解析 / 後退翼 / 乱流遷移 / 境界層 / プラズマ / 圧縮・非圧縮流 / 航空機空力デバイス / 空力制御デバイス / 空気力学 / 航空宇宙工学 / 空力デバイス / 航空機設計 / 流体力学 / 環境適合技術 / 航空宇宙流体力学 Less

甲虫翅構造の徹底的模倣による収納効率を極限まで高めた火星飛行機向け柔軟膜翼の提案Principal Investigator
- Principal Investigator
  
  金崎雅博
- Project Period (FY)
  2024 – 2026
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Tokyo Metropolitan University
Crossflow Reduction of Swept-Wing Boundary Layer and Delaying Turbulent Transition by Distributed Plasma Actuators
- Principal Investigator
  
  松野隆
- Project Period (FY)
  2022 – 2024
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Tottori University
Detailed Evaluation and Flow Structure Optimization for Applicable Knowledge Acquisition of Low-Speed/ High- Angle-of-Attack Aerodynamics of a Forward Swept WingPrincipal Investigator
- Principal Investigator
  
  Kanazaki Masahiro
- Project Period (FY)
  2021 – 2023
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Tokyo Metropolitan University
Time series aerodynamic control optimization for landing approach for supersonic aircraft subjected to unexpected turbulencePrincipal Investigator
- Principal Investigator
  
  Kanazaki Masahiro
- Project Period (FY)
  2016 – 2019
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Research Field
  
  Aerospace engineering
- Research Institution
  Tokyo Metropolitan University
Improvement of Multi-Electrode Plasma Actuator with Optimization of Discharge Parameters
- Principal Investigator
  
  Matsuno Takashi
- Project Period (FY)
  2015 – 2017
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Research Field
  
  Fluid engineering
- Research Institution
  Tottori University
Investigation on Aerodynamic Performance of Vertical Aileron
- Principal Investigator
  
  Imamura Taro
- Project Period (FY)
  2014 – 2015
- Research Category
  
  Grant-in-Aid for Challenging Exploratory Research
- Research Field
  
  Aerospace engineering
- Research Institution
  The University of Tokyo
Numerical Study on Digital Flight Simulation using Large-size Time-series Aerodynamic Data for Innovative Aerospace Vehicle DesignPrincipal Investigator
- Principal Investigator
  
  KANAZAKI Masahiro
- Project Period (FY)
  2013 – 2014
- Research Category
  
  Grant-in-Aid for Young Scientists (B)
- Research Field
  
  Intelligent informatics
- Research Institution
  Tokyo Metropolitan University
Development of High Power Plasma Actuator with a Novel Approach of Discharge Formation
- Principal Investigator
  
  MATSUNO Takashi
- Project Period (FY)
  2011 – 2012
- Research Category
  
  Grant-in-Aid for Young Scientists (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Tottori University

All 2023 2022 2020 2019 2018 2017 2016 2015 2014 2013 Other

All Journal Article Presentation

[Journal Article] Genetic Algorithm Applied to the Time-Series Landing Flight Path and Control Optimization of a Supersonic Transport2019
- Author(s)
  Kanazaki Masahiro、Saisyo Ryouta
- Journal Title
  
  The ACM International Conference Proceeding Series (ICPS), Association of Computing Machinery, NY, USA
  
  Volume: 0 Pages: 19-24
- DOI
  10.1145/3325773.3325789
- Peer Reviewed / Open Access
- Data Source
  KAKENHI-PROJECT-16K06888
[Journal Article] Multi-Fidelity Multi-Objective Efficient Global Optimization Applied to Airfoil Design Problems2017
- Author(s)
  Ariyarit Atthaphon、Kanazaki Masahiro
- Journal Title
  
  Applied Sciences
  
  Volume: 7 Issue: 12 Pages: 1318-1318
- DOI
  10.3390/app7121318
- Data Source
  KAKENHI-PROJECT-15K05797
[Journal Article] Hybrid surrogate-model-based multi-fidelity efficient global optimization applied to helicopter blade design2017
- Author(s)
  Ariyarit Atthaphon、Sugiura Masahiko、Tanabe Yasutada、Kanazaki Masahiro
- Journal Title
  
  Engineering Optimization
  
  Volume: 50 Issue: 6 Pages: 1016-1040
- DOI
  10.1080/0305215x.2017.1367391
- Data Source
  KAKENHI-PROJECT-15K05797
[Journal Article] Development of Multiobjective Trajectory-Optimization Method and Its Application to Improve Aircraft Landing2016
- Author(s)
  Othama, N., and Kanazaki
- Journal Title
  
  Aerospace Science & Technology
  
  Volume: 58 Pages: 166-177
- DOI
  10.1016/j.ast.2016.08.019
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-16K06888
[Journal Article] Optimum driving condition for lift creating cylinder by plasma actuators based on wind tunnel evaluation-based design2015
- Author(s)
  Kanazaki, M., Matsuno, T., Maeda, K, and Kawazoe, H.
- Journal Title
  
  International Journal of Automation and Logistics
  
  Volume: 2 Issue: 1/2 Pages: 45-59
- DOI
  10.1504/ijal.2016.074913
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-15K05797
[Journal Article] Development of Digital Flight Motion Methodology based on Aerodynamic Derivatives Approximation2015
- Author(s)
  Othama, N., and Kanazaki, M.
- Journal Title
  
  Journal of Robotics and Mechatronics
  
  Volume: Vol.27 No.5
- NAID
  130007671208
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-25870595
[Journal Article] Surrogate Model of Aerodynamic Model toward Efficient Digital Flight2015
- Author(s)
  Othama, N., and Kanazaki, M.
- Journal Title
  
  Procedia Engineering, Elsevier,
  
  Volume: 99 Pages: 703-712
- DOI
  10.1016/j.proeng.2014.12.592
- Peer Reviewed / Open Access
- Data Source
  KAKENHI-PROJECT-25870595
[Presentation] 大域的最適化法と直交格子ベースCFD "UTCart"を組み合わせた翼型設計2023
- Author(s)
  金崎雅博，今村太郎
- Organizer
  令和4年度航空宇宙空力シンポジウム
- Data Source
  KAKENHI-PROJECT-23K22953
[Presentation] 超音速前進翼の低速高迎角時の流れ構造に関する数値的研究2023
- Author(s)
  Armando, C., 金崎雅博
- Organizer
  第55回流体力学講演会／第41回航空宇宙数値シミュレーション技術シンポジウム
- Data Source
  KAKENHI-PROJECT-21K04480
[Presentation] 埋め込み境界法の特徴を利用した厚み0の翼型最適設計2022
- Author(s)
  金崎雅博，今村太郎
- Organizer
  第60回飛行機シンポジウム
- Data Source
  KAKENHI-PROJECT-23K22953
[Presentation] 埋め込み境界法を用いた数値流体力学を援用した空力形状最適設計効率化の試み2022
- Author(s)
  金崎雅博，今村太郎
- Organizer
  第38回ファジィシステムシンポジウム
- Data Source
  KAKENHI-PROJECT-23K22953
[Presentation] Low-speed high angle of attack forward-swept supersonic wing aerodynamic performance2022
- Author(s)
  Cuautle Armando，岸祐希，金崎雅博
- Organizer
  第60回飛行機シンポジウム
- Data Source
  KAKENHI-PROJECT-21K04480
[Presentation] 設計空間の縮約による多自由度形状の空力最適化2022
- Author(s)
  松野隆，樋口隆浩，岡田慎太郎，南角卓弥，金崎雅博
- Organizer
  日本機械学会第 14 回最適化シンポジウム 2022 (OPTIS2022)
- Data Source
  KAKENHI-PROJECT-23K22953
[Presentation] 二次元版UTCartと発見的探索法による形状融通性を活かした翼型最適設計フレームワーク2022
- Author(s)
  金崎雅博，今村太郎
- Organizer
  第35回計算力学講演会（CMD2022）
- Data Source
  KAKENHI-PROJECT-23K22953
[Presentation] "Low-Speed and High Angle of Attack Aerodynamic Characteristics of Supersonic Business Jet with Forward Swept Wing2020
- Author(s)
  Setoguchi, N, and Kanazaki, M.
- Organizer
  AIAA Scitech 2020 Forum, Orlando, FL, AIAA 2020-0534
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] RANS評価に基づく空力－飛行連成計算による超音速旅客機の着陸飛行経路最適化2019
- Author(s)
  最所諒大，金崎雅博，山田祐輔
- Organizer
  第51回流体力学講演会／第37回航空宇宙数値シミュレーション技術シンポジウ
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] Genetic Algorithm Applied to the Time-Series Landing Flight Path and Control Optimization of a Supersonic Transport2019
- Author(s)
  Kanazaki, M. and Saisho, R.
- Organizer
  2019 3rd International Conference on Intelligent Systems, Metaheuristics & Swarm Intelligence (ISMSI 2019)
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] Genetic Algorithm Applied to the Time-Series Landing Flight Path and Control Optimization of a Supersonic Transport2019
- Author(s)
  Kanazaki, M. and Saisho, R.
- Organizer
  2019 3rd International Conference on Intelligent Systems, Metaheuristics & Swarm Intelligence (ISMSI 2019), Male Maldives
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] 前進翼を持つSSBJの縦方向運動に対する動的空力特性調査2019
- Author(s)
  瀬戸口直，金崎雅博
- Organizer
  第51回流体力学講演会／第37回航空宇宙数値シミュレーション技術シンポジウ
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] SST着陸経路計算・最適設計のための空力―飛行力学連成計算について2018
- Author(s)
  金崎雅博，本間寛教，山田祐輔
- Organizer
  第５６回飛行機シンポジウム
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] EGO/MAs法を用いたプラズマアクチュエータ剥離抑制性能の最適化2017
- Author(s)
  橘一輝，松野隆，淺海典男，金崎雅博
- Organizer
  日本機械学会2017年度年次大会
- Data Source
  KAKENHI-PROJECT-15K05797
[Presentation] 「有翼ロケットにおける構成要素の組み合わせに対するオービタ・ブースタ抗力推算モデルの提案」2017
- Author(s)
  岩藤碩哉，金崎雅博，藤川貴弘，⽶本浩⼀
- Organizer
  第31回数値流体力学シンポジウム
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] 主翼上垂直舵翼の主翼コード長方向位置が空力性能に与える影響について2016
- Author(s)
  高梨聡、大森太加、砂田保人、今村太郎、金崎雅博、千葉一永、松野隆
- Organizer
  第47期日本航空宇宙学会年会講演会
- Place of Presentation
  東京都文京区東京大学山上会館
- Year and Date
  2016-04-14
- Data Source
  KAKENHI-PROJECT-26630440
[Presentation] エンジンインテーク統合設計における超音速翼の空力干渉の影響2016
- Author(s)
  岸祐希, 北崎慎哉, 牧野好和, 金崎雅博
- Organizer
  第30回数値流体力学シンポジウム2016
- Place of Presentation
  タワーホール船堀（東京都江戸川区）
- Year and Date
  2016-12-12
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] Trajectory and Aerodynamic Control Optimization of Civil Aircraft Descent Under Hazard Situations Based on High-Fidelity Aerodynamic Database2016
- Author(s)
  Othman, N. and Kanazaki, M.
- Organizer
  the 34th AIAA Applied Aerodynamics Conference, AIAA Aviation and Aeronautics Forum and Exposition 2016
- Place of Presentation
  Washington, D.C. (U. S. A.)
- Year and Date
  2016-06-05
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] Time-Series Optimization Methodology and Knowledge Discovery of Decend Trajectory for Civil Aircraft2016
- Author(s)
  Kanazaki, M. and Othman, N.
- Organizer
  IEEE Computational Intelligence Society (CIS), IEEE World Congress on Computational Intelligence
- Place of Presentation
  Vancouver (Canada)
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06888
[Presentation] Experimental Optimization of Plasma Aerodynamic Control and Their Flow Analysis2015
- Author(s)
  Takashi Matsuno, Masahiro Kanazaki, Kenichi Haruna, Gouji Yamada, Hiromitsu Kawazoe
- Organizer
  ASME-JSME-KSME Joint Fluids Engineering Conference 2015
- Place of Presentation
  Seoul, Korea
- Year and Date
  2015-07-27
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-15K05797
[Presentation] 主翼上垂直舵翼の平面形と空力特性の関係性に関する実験的研究2015
- Author(s)
  高梨聡、大森太加、砂田保人、今村太郎、金崎雅博、千葉一永、松野隆
- Organizer
  第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム
- Place of Presentation
  東京都目黒区　東京大学生産技術研究所駒場リサーチキャンパスAn棟
- Year and Date
  2015-07-02
- Data Source
  KAKENHI-PROJECT-26630440
[Presentation] 新しい空力デバイスとしての主翼上垂直フィンの可能性について2015
- Author(s)
  今村太郎、大森太加、高梨聡、砂田保人、金崎雅博、千葉一永、松野隆
- Organizer
  第53回飛行機シンポジウム
- Place of Presentation
  愛媛県松山市　松山市総合コミュニティセンター
- Year and Date
  2015-11-11
- Data Source
  KAKENHI-PROJECT-26630440
[Presentation] 航空機の突風応答緩和に向けた主翼上垂直舵面の利用に関する実験的研究2015
- Author(s)
  大森太加、高梨聡、今村太郎、砂田保人、金崎雅博、千葉一永、松野隆
- Organizer
  第53回飛行機シンポジウム
- Place of Presentation
  愛媛県松山市　松山市総合コミュニティセンター
- Year and Date
  2015-11-11
- Data Source
  KAKENHI-PROJECT-26630440
[Presentation] Efficient Global Optimization Applied to Aerodynamic Drag Reduction Around Cylinder Using Plasma Actuators in Wind Tunnel Experiment2015
- Author(s)
  Kanazaki, M., Matsuno, T., Maeda, K, and Kawazoe, H.
- Organizer
  IEEE Congress on Evolutionary Computation (CEC) 2015
- Place of Presentation
  Sendai, Japan
- Year and Date
  2015-05-25
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-15K05797
[Presentation] Unsteady Numerical Simulations of HTV-R Reentry Capsule by Using Detached-Eddy Simulation2014
- Author(s)
  Takii, K., Kanazaki, M., Ishiko, K., Hayashi, K., Hashimoto, A., and Aoyama, T.
- Organizer
  IAA Scitech2014, 52nd Aerospace Sciences Meeting (AIAA)
- Place of Presentation
  Washington D. C., U. S. A.
- Data Source
  KAKENHI-PROJECT-25870595
[Presentation] Design of Novel Wing Body Considering Intake/Exhaust Effects2013
- Author(s)
  Nakayama, Y., Kanazaki, M., Yotsuya, Y., and Matsushima, K.
- Organizer
  The 2013 Asia-Pacific International Symposium on Aerospace Technology (APISAT-2013)
- Place of Presentation
  Takamatsu, Japan
- Data Source
  KAKENHI-PROJECT-25870595
[Presentation] Efficient Design Exploration for Civil Aircraft Using a Kriging-Based Genetic2013
- Author(s)
  Kanazaki, M.
- Organizer
  EUROGEN 2013
- Place of Presentation
  Gran Canaria, Spain
- Invited
- Data Source
  KAKENHI-PROJECT-25870595
[Presentation] PREDICTION OF AERODYNAMIC COEFFICIENTS AND DERIVATIVES BY SURROGATE MODEL APPROACH2013
- Author(s)
  OTHMAN, N., and Kanazaki, M.
- Organizer
  ASIA-PACIFIC INTERNATIONAL CONGRESS ON ENGINEERING & NATURAL SCIENCES (APICENS) 2013
- Place of Presentation
  Taipei Taiwan
- Data Source
  KAKENHI-PROJECT-25870595
[Presentation] 並列評価計算が可能な環境下における Expected Improvement に基づく多数追加サンプルの獲得法と航空機翼端設計への応用
- Author(s)
  土屋陽祐，金崎雅博
- Organizer
  進化計算シンポジウム2014
- Place of Presentation
  広島県廿日市市安芸グランドホテル
- Year and Date
  2014-12-20 – 2014-12-21
- Data Source
  KAKENHI-PROJECT-26630440
[Presentation] High-fidelity ソルバを用いたフライトシミュレーション
- Author(s)
  1.金崎雅博
- Organizer
  航空宇宙流体科学サマースクール2014
- Place of Presentation
  福岡市
- Year and Date
  2014-08-05 – 2014-08-06
- Data Source
  KAKENHI-PROJECT-25870595
[Presentation] 主翼上垂直舵翼の平面形と空力特性の関係性に関する実験的研究
- Author(s)
  高梨聡,大森太加,砂田保人,今村太郎,金崎雅博,千葉一永,松野隆
- Organizer
  第４７回流体力学講演会／第３３回航空宇宙数値シミュレーション技術シンポジウム
- Place of Presentation
  東京　東京大学生産技術研究所
- Year and Date
  2015-07-02 – 2015-07-03
- Data Source
  KAKENHI-PROJECT-26630440
[Presentation] Efficient Flight Simulation Using Kriging Surrogate Model Based Aerodynamic Database
- Author(s)
  Othman, N, Kanazaki, M.
- Organizer
  AIAA SciTech2015
- Place of Presentation
  Kissimee, FL, USA.
- Year and Date
  2015-01-05 – 2015-01-09
- Data Source
  KAKENHI-PROJECT-25870595
[Presentation] Surrogate Model of Aerodynamic Model toward Efficient Digital Flight
- Author(s)
  Othman, N, Kanazaki, M.
- Organizer
  2014 Asia-Pacific International Symposium on Aerospace Technology
- Place of Presentation
  Shanghai, China
- Year and Date
  2014-09-24 – 2014-09-26
- Data Source
  KAKENHI-PROJECT-25870595

1. MATSUNO Takashi (90432608)

# of Collaborated Projects: 5 results

# of Collaborated Products: 10 results
2. 西田浩之 (60545945)

# of Collaborated Projects: 2 results

# of Collaborated Products: 0 results
3. Imamura Taro (30371115)

# of Collaborated Projects: 1 results

# of Collaborated Products: 5 results
4. CHIBA Kazuhisa (50450705)

# of Collaborated Projects: 1 results

# of Collaborated Products: 5 results
5. 永井大樹 (70360724)

# of Collaborated Projects: 1 results

# of Collaborated Products: 0 results

Kanazaki Masahiro 金崎 雅博

KANAZAKI Masahiro 金崎 雅博

Research Projects

Research Products

Co-Researchers

甲虫翅構造の徹底的模倣による収納効率を極限まで高めた火星飛行機向け柔軟膜翼の提案Principal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Crossflow Reduction of Swept-Wing Boundary Layer and Delaying Turbulent Transition by Distributed Plasma Actuators

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Detailed Evaluation and Flow Structure Optimization for Applicable Knowledge Acquisition of Low-Speed/ High- Angle-of-Attack Aerodynamics of a Forward Swept WingPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Time series aerodynamic control optimization for landing approach for supersonic aircraft subjected to unexpected turbulencePrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

Improvement of Multi-Electrode Plasma Actuator with Optimization of Discharge Parameters

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

Investigation on Aerodynamic Performance of Vertical Aileron

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

Numerical Study on Digital Flight Simulation using Large-size Time-series Aerodynamic Data for Innovative Aerospace Vehicle DesignPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

Development of High Power Plasma Actuator with a Novel Approach of Discharge Formation

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

[Journal Article] Genetic Algorithm Applied to the Time-Series Landing Flight Path and Control Optimization of a Supersonic Transport2019

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Multi-Fidelity Multi-Objective Efficient Global Optimization Applied to Airfoil Design Problems2017

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Hybrid surrogate-model-based multi-fidelity efficient global optimization applied to helicopter blade design2017

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[Journal Article] Development of Multiobjective Trajectory-Optimization Method and Its Application to Improve Aircraft Landing2016

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[Journal Article] Optimum driving condition for lift creating cylinder by plasma actuators based on wind tunnel evaluation-based design2015

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[Journal Article] Development of Digital Flight Motion Methodology based on Aerodynamic Derivatives Approximation2015

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Kanazaki Masahiro 金崎雅博

KANAZAKI Masahiro 金崎雅博