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Study on combustion instability

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24ECMP16 Subject Category: Competitive Funding PDF Responsible Representative: Seiji Tsutsumi, Research and Development Directorate, Research Unit III Contact Information: tsutsumi.seiji@jaxa.jp(tsutsumi.seiji@jaxa.jp) Members: Junya Aono, Masahito Akamine, Hiroyuki Ito, Seiji Tsutsumi Abstract In this study, LES analysis was carried out for Continuously Variable Resonant CoContinuously Variable (CVRC), and the contraction model which can predict the occurrence of vibration combustion was developed based on the obtained result, aiming at the prediction of vibration・・・<<read more>>

Development of technologies for hydrogen aircraft

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24ECMP25 Subject Category: Competitive Funding PDF Responsible Representative: Kenji Togami,team leader, Hydrogen Aircraft Core Technology Development Team Contact Information: Takuya Mitsukawa(mitsukawa.takuya@jaxa.jp) Members: Takuya Mitsukawa 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 high pressure hydrogen to the engine, and support product development by KHI and others.This work was supported・・・<<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 2024-January 2025 Report Number: R24ECMP26 Subject Category: Competitive Funding PDF Responsible Representative: Kazuyuki Nakakita, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub 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>>

Aerodynamic Performance and Aeroacoustic Analysis of Multi-Rotors

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24ECMP27 Subject Category: Competitive Funding PDF Responsible Representative: Kanako Yasue, Aviation Technology Directorate, Aviation Integration Innovation Hub Contact Information: Shigeru Sunada(shigeru.sunada@mae.nagoya-u.ac.jp) Members: Mahiro Iwaki, Fumihiro Kajiwara, Ryo Nishino, Hideaki Sugawara Abstract In recent years, aircraft electrification has been advancing in the aviation industry. A flight of an airplane with batteries is strongly disturbed with a wind, because they are small and light. We focus on an electric airplane having multiple・・・<<read more>>

Research and Development of Highly Efficient Propellers Covering a Wide Range of Speeds

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24ECMP28 Subject Category: Competitive Funding PDF Responsible Representative: Masashi Harada, Aeronautical Thechnology Directorate, Aviation Safety Innovation Hub Contact Information: Mizue Munekata, Kumamoto Univercity(munekata@gpo.kumamoto-u.ac.jp) Members: Mizue Munekata, Junnosuke Suganuma Abstract Currently, SLT is developing a tilt-wing VTOL aircraft. It is necessary to develop a propeller that can demonstrate high efficiency over a wide range of speeds from low to high to meet the requirements of this aircraft. The propeller is designed・・・<<read more>>