Rchr
J-GLOBAL ID：201701004939333351   Update date: Jul. 23, 2024

Takehiro Himeno

ヒメノ タケヒロ | Takehiro Himeno
Affiliation and department：
The University of Tokyo

About The University of Tokyo


Research field  (1)： Aerospace engineering
Research theme for competitive and other funds  (11)：
  • 2021 - 2026 Fundamental Study on Cryogenic Fluid Management for the Design of Orbital Transfer Vehicles and Propellant Depot Systems
  • 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
Show all
Papers (142)：
  • Osamu Kawanami, Kentaro Takeda, Ryoki Matsushima, Ryoji Imai, Yutaka Umemura, Takehiro Himeno. Estimation of the tip-height of mixing jet issuing from a nozzle by one-dimensional droplet model. International Journal of Multiphase Flow. 2023. 163. 104426-104426
  • Yutaro Furuichi, Takehiro Himeno, Toshinori Watanabe, Mitsuhisa Baba, Masatsugu Otsuki. Evaluation of Sloshing Effect on a Tank during Landing Phases of Spacecrafts in a Micro-Gravity Environment. ASCEND 2022. 2022
  • Osamu KAWANAMI, Kentaro TAKEDA, Ryoki MATSUSHIMA, Ryoji IMAI, Yutaka UMEMURA, Takehiro HIMENO. Observation of Flow Pattern and Jet-tip Height Issuing from a Nozzle at Tank Bottom in Microgravity. International Journal of Microgravity Science and Application. 2022. 39. 2. 390201
  • Yuji Tanaka, Mitsuhisa Baba, Masatsugu Otsuki, Kazuhisa Fujita, Takehiro Himeno, Takao Maeda, Masaki Takahashi. Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity. Proceedings of the IEEE Conference on Decision and Control. 2022. 2022-December. 3092-3097
  • Jiuliang Gan, Toshinori Watanabe, Takehiro Himeno. Effect of shock wave behavior on unsteady aerodynamic characteristics of oscillating transonic compressor cascade. Proceedings of the ASME Turbo Expo. 2021. 9
ｍore...
MISC (31)：
ｍore...
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)
ｍore...
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
Show all
※ Researcher’s information displayed in J-GLOBAL is based on the information registered in researchmap. For details, see here.

Return to Previous Page

TOP

BOTTOM