Rchr
J-GLOBAL ID:201501016995926911   Update date: Jan. 17, 2024

Terashima Hiroshi

テラシマ ヒロシ | Terashima Hiroshi
Affiliation and department:
Job title: 准教授
Homepage URL  (1): https://kaken.nii.ac.jp/d/r/20415235.ja.html
Research field  (5): Computational science ,  Aerospace engineering ,  Thermal engineering ,  Safety engineering ,  Social systems engineering
Research keywords  (5): 数値流体力学 ,  燃焼反応流体 ,  超臨界流体 ,  気液界面 ,  空力弾性
Research theme for competitive and other funds  (14):
  • 2021 - 2024 超臨界圧燃焼流れ場の高度デジタル予測に資する詳細反応機構-燃焼LES技術の開発
  • 2022 - 2024 詳細反応機構-超臨界圧燃焼LES解析を可能とする乱流燃焼モデルの開発
  • 2019 - 2022 Challenges for high-fidelity turbulent combustion simulation based on detailed reaction mechanisms
  • 2017 - 2020 Modeling for multi-component flows and combustion dynamics under supercritical pressure environments
  • 2015 - 2018 Combustion-reaction database specialized for accidental fire/explosion simulations
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Papers (67):
  • NAKATSUKASA Tomohito, AMANO Taishi, ARAKI Takahide, TERASHIMA Hiroshi, TSUBOI Nobuyuki, OZAWA Kohei. Numerical Study of Cryogenic Hydrogen Jet in Crossflow under Supercritical Pressure: Comparison of Tandem and Twin Jets. Journal of Evolving Space Activities. 2023. 1. n/a
  • Toma Miyake, Hiroshi Terashima. Numerical Investigation of Transonic Flutter Characteristics of a Supercritical Airfoil. Lecture Notes in Electrical Engineering. 2023. 912. 607-621
  • Noah D. Oyeniran, Hiroshi Terashima. A Computational Study on Unsteady Aerodynamic Forces Around a Pitching Airfoil with Shock and Shock-Induced Separation. Lecture Notes in Electrical Engineering. 2023. 912. 353-360
  • Noah D. Oyeniran, Toma Miyake, Hiroshi Terashima, Ryoto Seki, Keiichi Ishiko, Taku Nonomura. Unsteady Aerodynamics Around a Pitching Airfoil with Shock and Shock-Induced Boundary-Layer Separation. AIAA Journal. 2022
  • Toru Ota, Hiroshi Terashima, Nobuyuki Oshima. Mechanisms for severe combustion instabilities induced by low-temperature fuel injection of an H2/O2 rocket-type combustor. AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. 2022
more...
MISC (75):
  • 大島 伸行, 寺島 洋史. 『富岳』燃焼シミュレーションに向けての数値モデルと計算法-Numerical Models and Methods for Combustion Simulation on FUGAKU Class Supercomputer-特集 燃焼科学における大規模数値シミュレーションの最前線. 日本燃焼学会誌 = Journal of the Combustion Society of Japan. 2022. 64. 208. 136-143
  • KAWARAI Yuki, TERASHIMA Hiroshi. Accelerating the calculation of supercritical non-ideal thermal and transport property models using deep learning. The Proceedings of Mechanical Engineering Congress, Japan. 2022. 2022. J061-03
  • 鶴本徹, 高橋裕介, 寺島洋史, 大島伸行. Study on Aerodynamic Instability Mitigation for Hayabusa-type Reentry Capsule using Proper Orthogonal Decomposition. 衝撃波シンポジウム講演論文集(CD-ROM). 2020. 2019
  • 太田徹, 寺島洋史, 大島伸行. A mechanism for injection coupled combustion instabilities of an H2/O2 rocket-type combustor. 数値流体力学シンポジウム講演論文集(CD-ROM). 2020. 34th
  • 大江真央, 寺島洋史, 林潤, 赤松史光, 大島伸行. Flame Holding/Extinguishing Mechanisms for Ammonia and Methane Laminar Non-premixed Jet Flames. 数値流体力学シンポジウム講演論文集(CD-ROM). 2020. 34th
more...
Books (2):
  • High-pressure flows for propulsion applications
    American Institute of Aeronautics and Astronautics 2020 ISBN:9781624105807
  • 1) 計算力学ハンドブック「第II巻 差分法・有限体積法(熱流体編)」
    日本機械学会,丸善 2006
Lectures and oral presentations  (30):
  • A computational study for combustion flow fields of a high-pressure gaseous hydrogen/oxygen coflow jet behind a splitter plate
    (AIAA Scitech 2019 Forum 2019)
  • 定容容器におけるエンドガス局所自着火現象の可視化
    (日本伝熱シンポジウム講演論文集(CD-ROM) 2017)
  • 柔軟構造体に対する再突入ブラックアウトの数値解析
    (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) 2017)
  • 観測ロケットを用いた柔軟構造体の再突入試験における空力不安定性解析
    (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) 2017)
  • Numerical simulation for effects of pressure on cryogenic coaxial jet under supercritical pressure
    (AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting 2017)
more...
Education (3):
  • 2000 - 2004 The University of Tokyo
  • 1998 - 2000 Tohoku University
  • 1994 - 1998 Tohoku University Faculty of Engineering
Professional career (1):
  • Ph.D.
Work history (8):
  • 2023/04 - 現在 Stanford University Department of Mechanical Engineering Visiting associate professor
  • 2015/12 - 現在 Hokkaido University Faculty of Engineering Associate Professor
  • 2013/04 - 2015/11 University of Tokyo School of Engineering Project Associate Professor
  • 2011/04 - 2013/03 The University of Tokyo
  • 2009/04 - 2011/03 JAXA JEDI Aerospace Project Researcher
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Awards (1):
  • 2016 - 日本燃焼学会 平成28年度日本燃焼学会 奨励賞
Association Membership(s) (5):
AIAA ,  THE JAPAN SOCIETY OF FLUID MECHANICS ,  COMBUSTION SOCIETY OF JAPAN ,  THE JAPAN SOCIETY OF MECHANICAL ENGINEERS ,  THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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