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Development of technologies for hydrogen aircraft

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25ECMP25 Subject Category: Competitive Funding PDF Responsible Representative: Kenji Togami,team leader, HY-FLARE Project Team (Hydrogen Combustor Facility and Cryogenic Liquid Pump Research and Development for Advanced Hydrogen Aircraft Project Team) Contact Information: Takuya Mitsukawa(mitsukawa.takuya@jaxa.jp) Members: Yutaka Kusaka, Takuya Mitsukawa, Hitoshi Arizono Abstract According to the specifications of hydrogen aircraft, we prototype and test a "boost pump" to pump up liquid hydrogen from a tank and an "engine pump" to supply・・・<<read more>>

Efficient spatial second-order precision compressible fluid calculation method with resolution equivalent to fifth-order precision

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25ECMP26 Subject Category: Competitive Funding PDF Responsible Representative: Kazuyuki Nakakita, Aviation Technology Directorate, Fundamental Technology Research Unit Contact Information: Andrea Sansica(sansica.andrea@jaxa.jp) Members: Haruyuki Kakimoto, Keiichi Kitamura, Tomohiro Mamashita, Sora Yasui, David Lusher, Andrea Sansica Abstract In this study, we move from the MUSCL framework and use the MUSCL-THINC method, which gives the physical quantity distribution within a numerical cell as a hyperbolic function, allowing to sharply capture shock wave discontinuities.・・・<<read more>>

A study on design of engines with a wide range operation

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25ECMP36 Subject Category: Competitive Funding PDF Responsible Representative: Hideaki Nanri, Research and Development Directorate, Research Unit IV Contact Information: Shun Takahashi Research and Development Directorate, Research Unit IV(takahashi.shun@jaxa.jp) Members: Mika Edahiro, Masaaki Fukui, Chihiro Fujio, Kaito Hirose, Kosuke Hamaji, Yuki Hirayama, Taku Inoue, Ryota Kobayashi, Noriko Katsumura, Kota Matsuhashi, Toshihiko Munakata, Kei Norimatsu, Koutarou Nakayama, Shinji Nakaya, Ikuo Ozawa, Takuma Tadokoro, Shunsuke Takamatsu, Masahiro Takahashi, Shun Takahashi, Takuto Yamaguchi Abstract・・・<<read more>>

On development of aircraft noise control method based on resolvent analysis

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25ECMP77 Subject Category: Competitive Funding PDF Responsible Representative: Kazuyuki Nakakita, Aeronarutical Technology Directorate, Fundamental research unit Contact Information: Yoimi Kojima(kojima.yoimi@jaxa.jp) Members: Yoimi Kojima Abstract This study aims to develop an efficient method for total temperature suppression using the resolvent analysis method, a technique for analyzing the linear response characteristics of flow. By leveraging resolvent analysis, the goal is to shorten the aircraft noise reduction process, which has traditionally required extensive・・・<<read more>>

Research on plasma analysis method in electric propulsion

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25ECWU04 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Yasuhiro Mizobuchi, Project Manager, Aviation Technology Directorate, Aircraft Digital Transformation Technology Demonstration (XANADU) Project Team Contact Information: Kiyoshi Kinefuchi, Department of Aerospace Engineering, Graduate School of Engineering, Nagoya University(kiyoshi.kinefuchi@mae.nagoya-u.ac.jp) Members: Satoshi Inoue, Masaki Yamaguchi Abstract The objective of this study is to understand plasma physics phenomena in electric propulsion systems such as hollow cathode and MPD thruster. In order to・・・<<read more>>

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