Rchr
J-GLOBAL ID:201701004939333351   Update date: Oct. 24, 2021

Takehiro Himeno

ヒメノ タケヒロ | Takehiro Himeno
Affiliation and department:
Research field  (1): Aerospace engineering
Research theme for competitive and other funds  (11):
  • 2021 - 2026 極低温ロケット高度化と軌道上再補給に関わる熱流動現象解明と予測技術の総合的研究
  • 2018 - 2021 Cryogenic Propellant Management with Phase Change for Liquid Rocket Sysyems
  • 2015 - 2018 Thermal-fluid Behavior of Two-phase flows for Propellant Management in Upper Stage Propulsion System
  • 2014 - 2018 Structural and fluidic investigation and instability suppression mechanism in the configuration of tip-driven electric fan for aircraft
  • 2012 - 2015 Investigation on two-phase flows for the Innovation of Cryogenic Upper Stage
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Papers (130):
  • 姫野武洋, 渡辺紀徳. Feasibility Study of TeDP based on Engine-Cycle Analysis and Weight Estimation. 日本ガスタービン学会誌. 2021. 49. 1
  • Kazuma Tani, Takehiro Himeno, Yasunori Sakuma, Toshinori Watanabe, Hiroaki Kobayashi, Terukuni Toge, Syuntaro Unno, Shoji Kamiya, Osamu Muragishi, Katsuhiro Kanbe. Pressure recovery during pressure reduction experiment with large-scale liquid hydrogen tank. International Journal of Hydrogen Energy. 2021
  • Kiyoshi Kinefuchi, Hideto Kawashima, Daizo Sugimori, Yutaka Umemura, Koichi Okita, Hiroaki Kobayashi, Takehiro Himeno. Experimental analysis of thermal behavior in cryogenic propellant tank with different pressurants. CRYOGENICS. 2020. 112
  • Ryoji Imai, Kazuaki Nishida, Osamu Kawanami, Yutaka Umemura, Takehiro Himeno. Ground based experiment and numerical calculation on thermodynamic vent system in propellant tank for future cryogenic propulsion system. CRYOGENICS. 2020. 109
  • Ryoji Imai, Kazuaki Nishida, Osamu Kawanami, Yutaka Umemura, Takehiro Himeno. Basic Study on Thermodynamic Vent System in Propulsion System for Future Spacecraft. MICROGRAVITY SCIENCE AND TECHNOLOGY. 2020. 32. 3. 339-348
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MISC (28):
  • 今井良二, 河南治, 梅村悠, 姫野武洋. Study on break of thermal stratification in container targeted to thermodynamic vent system for future spacecraft. 混相流シンポジウム講演論文集(Web). 2018. 2018
  • 世古口直也, 渡辺紀徳, 姫野武洋, 井上智博, 鵜沢聖治, 佐久間康典, 富田進, 渡辺和嗣. フィン周囲流れ場に着目したサーフェスクーラの放熱特性に関する数値解析. 航空原動機・宇宙推進講演会講演論文集(CD-ROM). 2015. 55th
  • 井上智博, 渡辺紀徳, 姫野武洋, 鵜沢聖治. 多噴射器環境下の衝突微粒化. 微粒化シンポジウム講演論文集. 2015. 24th
  • 佐久間康典, 渡辺紀徳, 姫野武洋, 加藤大, 室岡武, 周藤由香里. 異なる翼端間隙高さを有する遷音速ファンに周方向溝型ケーシングトリートメントが及ぼす影響. 日本機械学会計算力学講演会論文集(CD-ROM). 2014. 27th
  • Kinefuchi Kiyoshi, Saitoh Yasuhiro, Nishihira Shintaro, Sarae Wataru, Sugimori Daizo, Okita Koichi, Tani Naoki, Umemura Yutaka, Kobayashi Hiroaki, Himeno Takehiro, et al. H2A Upper Stage Evolution to Contribute to the Exploration-R&D Activities of Cryogenic Propulsion Stage-. 2013
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Lectures and oral presentations  (232):
  • Cfd modeling of phase change and pressure drop during violent sloshing of cryogenic fluid in a small-scale tank
    (AIAA Propulsion and Energy 2020 Forum 2020)
  • Cfd modeling of cryogenic chilldown in a complex channel under normal and low gravity conditions
    (AIAA Propulsion and Energy 2020 Forum 2020)
  • Numerical Research on Pressure Recovery During Depressurization Inside Large-Scale Liquified Hydrogen Tank
    (数値流体力学シンポジウム講演論文集(CD-ROM) 2020)
  • Feasibility Study of Electric Propulsion for Aircraft based on Engine-Cycle Analysis and Weight Estimation
    (飛行機シンポジウム講演集(CD-ROM) 2020)
  • Studies on Thermodynamic Vent System for Cryogenic Propellant Storage Tank. (Evaluation Test of Jet Mixing with Self Pressurization)
    (宇宙科学技術連合講演会講演集(CD-ROM) 2020)
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Awards (6):
  • 2020/04 - The Gas Turbine Society of Japan GTSJ Medal for Outstanding Paper
  • 2018/04 - The Gas Turbine Society of Japan GTSJ Medal for Outstanding Paper Verification and Application of Fluid-Structure Interaction and a Modal Identification Technique to Cascade Flutter Simulations
  • 2012/07 - American Institute of Aeronautics and Astronautics (AIAA) AIAA Liquid Propulsion Best Paper Award
  • 2012/04 - Japan Society of Mechanical Engineers JSME Medal for Outstanding Paper
  • 2008/07 - American Institute of Aeronautics and Astronautics (AIAA) AIAA Liquid Propulsion Best Paper Award Numerical and Experimental Investigation on Sloshing in Rocket Tanks with Damping Devices
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