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Aerodynamic testing technology for reentering capsules

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EA1403 Subject Category: Aeronautical Technology PDF Responsible Representative: Shigeru Hamamoto, Aviation Technology Directorate, Aeronautical Facility Research Unit Contact Information: Keisuke Fujii(fujii.keisuke@jaxa.jp) Members: Keisuke Fujii, Hiroya Toriida, Hidemi Takahashi, Yoshiki Takama, Takahiro Yamamoto Abstract To enhance hypersonic aerodynamic testing technology especially for reentering vehicles through developing understanding about the hypersonic wind tunnel nozzle flow which affects a lot estimation error to the flight characteristics and through defining the ability in predicting・・・<<read more>>

Investigation of internal flow of aircraft combustor for En-Core Project.

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EA0714 Subject Category: Aeronautical Technology PDF Responsible Representative: Mitsumasa Makida(JAXA, Aeronautical Technology Directorate) Contact Information: Mitsumasa Makida(JAXA, Aeronautical Technology Directorate)(makida.mitsumasa@jaxa.jp) Members: Naoki Nakamura, Mitsumasa Makida, Takashi Ishiyama Abstract In the development process of aircraft combustors, air mass flow distribution between fuel nozzles, dilution and cooling air holes on the liner effects performances of combustors. So it is important to understand the internal flow and estimate the mass flow distribution. In・・・<<read more>>

Research on Aircraft Multidisciplinary Design Technology

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EA0602 Subject Category: Aeronautical Technology PDF Responsible Representative: Dongyoun Kwak, Aviation Enviromental Sustanability Innovation Hub, Aviation Technology Directorate Contact Information: Mitsuhiro Murayama, Aviation Environmental Sustainability Innovation Hub, Aviation Technology Directorate(murayama.mitsuhiro@jaxa.jp) Members: Ryutaro Furuya, Tomoaki Ikeda, Yasushi Ito, Fumitake Kuroda, Keisuke Ohira, Yuki Kishi, Dongyoun Kwak, Mitsuhiro Murayama Abstract The purpose of the research is to develop and mature a bunch of advanced and innovative elemental technologies on aerodynamics, aeroacoustics, and・・・<<read more>>

Research on laminar fins system

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EA0601 Subject Category: Aeronautical Technology PDF Responsible Representative: Dongyoun Kwak, Hub Maneger, Aviation Environmental Sustainability Innovation Hub/Aviation Technology Directorate Contact Information: Naoko Tokugawa(tokugawa.naoko@jaxa.jp) Members: Takahiro Ishida, Keisuke Ohira, Naoko Tokugawa, Keiji Ueshima, Hayahide Yoshida, Shota Yamamoto, Koki Miyata Abstract The laminar flow vertical tail fins are designed and evaluated to establish practical technology for a natural laminar flow wing that will be applied to future subsonic aircraft. By investigating the・・・<<read more>>

JSS3 TOKI-SORA ranked in major benchmark results

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We are happy to inform all of you the news that TOKI-SORA, main computing resource of our JSS3 supercomputer system, is ranked in major supercomputer benchmark results (November 14, 2023). TOP500: Ranked as 53rd. (November 2023) Reference: TOP500 » November 2023 HPCG: Ranked as 17th. (November 2023) Reference: HPCG – November 2023 Graph500: Ranked as 7th. (November 2023 BFS) Reference: Graph 500 – November 2023 BFS