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Research and development of prediction technology for thermal and aerodynamic characteristics of hypersonic vehicle

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G20 Subject Category: Aeronautical Technology PDF Responsible Representative: Yasuhiro Mizobuchi, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: matsuyama.shingo@jaxa.jp(matsuyama.shingo@jaxa.jp) Members: Keisuke Fujii, Shingo Matsuyama, Hidemi Takahashi, Takahiro Yamamoto Abstract Strong shock waves are generated around a flying object at hypersonic speeds, and the high-temperature gas compressed by the shock waves causes strong heat transfer to the hypersonic vehicle. The objective of this research is to establish a technique to・・・<<read more>>

Integrated simulation over aircraft, rotorcraft and engines

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G21 Subject Category: Aeronautical Technology PDF Responsible Representative: Atsushi Hashimoto, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Kanako Yasue(yasue.kanako@jaxa.jp) Members: Hirokazu Higashida, Manabu Hisida, Atsushi Hashimoto, Mami Hayakawa, Kenji Hayashi, Tomoaki Ikeda, Takashi Ishida, Masatoshi Kanayama, Ryohei Kirihara, Masashi Kanamori, Takuhito Kuwabara, Yuichi Matsuo, Shingo Matsuyama, Yasuhiro Mizobuchi, Taisuke Nambu, Hideji Saiki, Kei Shimura, Atsushi Shinozuka, Andrea Sansica, Shota Taniguchi, Kanako Yasue, Hiroki Yao Abstract An aircraft is・・・<<read more>>

Development of Aeroelastic Simulation Tool based on FaSTAR-Move

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G02 Subject Category: Aeronautical Technology PDF Responsible Representative: Hitoshi Arizono, Aircraft Lifecycle Innovation Hub Contact Information: Hitoshi Arizono(arizono.hitoshi@jaxa.jp) Members: Hitoshi Arizono, Kohei Konishi, Hamidreza Kheirandish Abstract Development of Aeroelastic Simulation Tool based on FaSTAR-Move Reference URL N/A Reasons and benefits of using JAXA Supercomputer System Aeroelastic analysis requires unsteady analysis. Therefore, it is necessary to use JSS2 because the simulation cost is high. Achievements of the Year Inplemented the moving・・・<<read more>>

High-Reynolds number stall characteristics of a wing-body configuration model

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G10 Subject Category: Aeronautical Technology PDF Responsible Representative: Kazuyuki Nakakita, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Kazuyuki Nakakita, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub(nakakita.kazuyuki@jaxa.jp) Members: Kuniyuki Takekawa, Takahiro Yamamoto Abstract Aerodynamic characteristics of a fundamental wing-body configuration model was analyzed by CFD to compare with High-Reynolds number wind tunnel data conducted in JAXA’s collabollation research. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>

Research on Particle Simulation Methods

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G19 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aviation Technology Directorate, Program Director Contact Information: Kenichi Kubota, Aircraft Lifecycle Innovation Hub, Aviatoin Technology Directorate(kubota.kenichi@jaxa.jp) Members: Kenichi Kubota, Keita Nakamoto Abstract The purpose of this research is to obtain the simulation technology of particle simulation, known to be useful for analysing multi-physics phenomena, to accelerate aircraft development. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System JSS3・・・<<read more>>