Curriculum Vitaes
Profile Information
- Affiliation
- Professor, Institute of Space and Astronautical Science, JAXA
- Degree
- 工学博士(東京大学)
- J-GLOBAL ID
- 200901061542880861
- researchmap Member ID
- 5000019456
Research History
8-
Apr, 2022 - Present
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Feb, 2022 - Present
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Feb, 2017 - Jan, 2022
Education
1-
- 2001
Committee Memberships
2Papers
174-
Applied Thermal Engineering, 126218-126218, Mar, 2025
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Cryogenics, 131 103652-103652, Apr, 2023
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IEEE Transactions on Applied Superconductivity, 2023
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IEEE Transactions on Applied Superconductivity, 32(6) 1-5, 2022 Peer-reviewed
Misc.
170-
宇宙航空研究開発機構研究開発資料 JAXA-RM-, (12-001), 2012
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2010(45) 200-201, Mar 12, 2010
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2010 14-14, 2010The wake flow of fuel injection strut was experimentally investigated, which simulates cold flow field inside of the Pre-cooled turbojet engine's afterburner, by means of schlieren photographing, PIV measurement, and hot-wire anemometry. In previous study, the large scale Karman vortex sheets were observed behind the struts and large scale turbulent mixing was enhanced by them. In this study, experiments were carried out in various fuel injection pressure cases, and it is clarified that the fuel didn't enter into recirculation region behind strut, or flame holding region, on high fuel injection pressure case, because of the increasing of the penetration of fuel jet.
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 50th, 2010
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 50th, 2010
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 50th, 2010
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81 60-60, Nov 18, 2009
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2009 322-322, 2009JAXA has been developing the Pre-Cooled turbojet engine with afterburner for hypersonic aircraft. The afterburner will work on super/hypersonic speed to increase the thrust. However, its combustion efficiency is not enough for practical use. To improve the performance of the afterburner, it is necessary to clarify the details of the flow field. Therefore we designed the wind tunnel that can simulate the flow field inside of the afterburner and carried out the PIV measurements, the hot-wire measurements and the flow visualization by Schlieren optical system. The results showed that there was Karman vortex sheet behind the flame-holding strut and its large coherent structures were still kept toward the downstream of the flow.
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Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan (Web), 7(ists26), 2009
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Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan (Web), 7(ists26), 2009
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60th International Astronautical Congress 2009, IAC 2009, 8, 2009
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16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 49th, 2009
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宇宙航空研究開発機構特別資料 JAXA-SP-, (08-009), 2009
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15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2008
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15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2008
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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, 40th-2008, 2008
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日本マイクログラビティ応用学会誌, 24(3), 2007
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International Astronautical Federation - 58th International Astronautical Congress 2007, 9, 2007
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 47th, 2007
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宇宙科学技術連合講演会講演集(CD-ROM), 51st, 2007
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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, 39th-2007, 2007
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航空原動機・宇宙推進講演会講演論文集(CD-ROM), 47th, 2007
Presentations
64-
The Proceedings of Mechanical Engineering Congress, Japan, 2018<p>A loading system plays a role of loading and unloading liquid hydrogen between a carrier ship and a ground storage facility in hydrogen supply chain in which hydrogen in the form of liquid phase is transported by the carrier ship from a resource-rich country to a consuming country. An emergency release system (ERS), which is one of components of the loading system, is installed in the middle of transfer pipe of the loading system, and has function of separating and plugging the pipe at an abnormality during loading so as to prevent a large amount of cryogenic fluid from scattering. We have conducted R & D study of the ERS for liquid hydrogen based on an existing one for liquid natural gas (LNG). Whole system function of the ERS including separation behavior was verified conducting a field experiment with the ERS test model and liquid hydrogen. Through several tests, the separation mechanism and behavior were verified, and also, soundness of the seal mechanism was evaluated. While, auto-ignition phenomena were observed on the separation surface of the ERS after the separation, of which causes have not been identified yet. Characteristics of dispersion behavior of hydrogen that was released at the separation could be investigated measuring distribution of temperature and hydrogen concentration around the ERS test model.</p>
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The Proceedings of Mechanical Engineering Congress, Japan, 2018<p>To improve safety regulations for fuel cell vehicles and hydrogen infrastructure, experiments of cryo-compressed hydrogen leakage diffusion were conducted. The experimental apparatus can supply 90 MPa hydrogen of various temperature conditions. Measurement items were hydrogen concentration distribution, blast pressure, flame length, and radiant heat. In addition, high speed camera observation was carried out to investigate the near-field of cryogenic hydrogen jet at supercritical pressure. The experimental apparatus can supply 90 MPa hydrogen at various temperature conditions (50 K–300 K) at a maximum flow rate of 100 kg/h. The hydrogen leakage flow rate was measured using pinhole nozzles with different outlet diameters (0.2 mm, 0.4 mm, 0.7 mm, and 1 mm). It was confirmed that the hydrogen leakage flow rate increases as the supply temperature decreases. The hydrogen concentration distribution was measured by injecting high-pressure hydrogen from the 0.2-mm pinhole for 10 min under a constant pressure/temperature condition. As the hydrogen injection temperature decreased, it was found that the hydrogen concentration increased, and an empirical formula of the 1% concentration distance for the cryogenic hydrogen system was newly presented.</p>
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日本冷凍空調学会年次大会講演論文集 Proceedings of the JSRAE Annual Conference, 2017
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The Proceedings of Mechanical Engineering Congress, Japan, 2017
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The Proceedings of Mechanical Engineering Congress, Japan, 2017<p>JAXA has constructed an experimental facility to pressurize and supply liquid hydrogen at a maximum pressure of 90 MPa to conduct experimental research on the injection of high pressure liquid hydrogen into the atmosphere. Liquid hydrogen has a property that its density greatly changes depending on pressure despite being a liquid phase. In addition, the high pressure hydrogen gas is in a supercritical state and has an intermediate property between a gas and a liquid. Therefore, it is a difficult question whether to treat the injection of high pressure liquid hydrogen as a gas phase phenomena or as a liquid phase phenomena. As a result of the experiment, it was found good to apply the liquid orifice equation to predict the discharge flow rate of high pressure liquid hydrogen.</p>
Professional Memberships
3-
Apr, 2019 - Present
Research Projects
14-
Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2024 - Mar, 2027
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科学研究費助成事業, 日本学術振興会, Apr, 2023 - Mar, 2027
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科学研究費助成事業, 日本学術振興会, Apr, 2020 - Mar, 2023
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2019 - Mar, 2022
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2015 - Mar, 2018