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Development of improved numerical tools for Certification by Analysis(CbA)

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G22 Subject Category: Aeronautical Technology PDF Responsible Representative: Kazuyuki Nakakita, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Andrea Sansica(sansica.andrea@jaxa.jp) Members: Hirokazu Higashida, Manabu Hisida, Atsushi Hashimoto, Kenji Hayashi, Yuki Ide, Takashi Ishida, Masashi Kanamori, David Lusher, Tomoaki Matsuzaki, Yoimi Kojima, Hideji Saiki, Yosuke Sugioka, Andrea Sansica, Kosuke Uchida, Takahiro Yamamoto, Paul Zehner, Markus Zauner Abstract High-accuracy simulations for stall and buffet are needed during the aircraft design. However,・・・<<read more>>

Research on low-cost LES and one-dimensional model for aeroengine combustor

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G23 Subject Category: Aeronautical Technology PDF Responsible Representative: Yasuhiro Mizobuchi, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Shingo Matsuyama(matsuyama.shingo@jaxa.jp) Members: Masanori Harada, Nagayoshi Hiromitsu, Kotaro Iguchi, Yuta Kusakabe, Hideki Moriai, Koutarou Munenaga, Shingo Matsuyama, Taisei Miyoshi, Yuichi Taniguchi Abstract There is a strong need to incorporate LES that can reproduce combustion phenomena with high fidelity into the design process to improve the efficiency of combustor development for aero・・・<<read more>>

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>>