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Hydrogen Application to Aircraft and Future Space Transportation System

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EA2121 Subject Category: Aeronautical Technology PDF Responsible Representative: Sadatake Tomioka, Leader, Hydrogen Aerospace Plane Team Contact Information: Hideyuki Taguchi(taguchi.hideyuki@jaxa.jp) Members: Koichi Omi, Manami Fujii, Yuki Kuwabara, Rintaro Tanaka, Koutarou Nakayama, Shota Kiuchi, Nozomi Takaki, Shima Ariyoshi, Aoto Kikui, Kaito Hirose, Ryo Yoshida, Shunsuke Takamatsu, Tomofumi Narita, Shinji Nakaya, Masafumi Momose, Taisuke Nambu, Naoyuki Okamura, Junichi Oki, Shunsuke Imamura, Motoyuki Hongoh, Hideyuki Taguchi Abstract This research aims at the demonstration of・・・<<read more>>

Improvement of numerical analysis for internal flow with complicated configuration inside aero-engine

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EA2120 Subject Category: Aeronautical Technology PDF Responsible Representative: ISHII Tatsuya, Director, Aviation Technology Directrate, Aviation Environmental Sustainability Innovation Hub Contact Information: Taisuke Nambu, Aviation Technology Directorate, Aviation Environmental Sustainability Innovation Hub(nambu.taisuke@jaxa.jp) Members: Takashi Aoyama, Shunji Enomoto, Atsushi Hashimoto, Kenji Hayashi, Takashi Ishida, Masatoshi Kanayama, Junichi Kazawa, Takahisa Kohno, Mitsumasa Makida, Taisuke Nambu, Hiroki Ugajin, Kanako Yasue Abstract Unstructured-grid flow solver FaSTAR-Move-AE are applied to aero-engine analysis with complicated configuration. Through・・・<<read more>>

Research on Structure and Composite Material Technologies for Digital Certification

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EA1601 Subject Category: Aeronautical Technology PDF Responsible Representative: Yuichiro Aoki, Senior Researcher, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Yuichiro Aoki, Digital Structures and Materials Technology Team, Aircraft Lifecycle Innovation Hub, Aviation Technology Directorate(aoki.yuichiro@jaxa.jp) Members: Hiroyuki Akiyama, Yuichiro Aoki, Makoto Goto, Yoshiyasu Hirano, Shinsaku Hisada, Kenichi Kubota, Shintaro Kamiyama, Toshiyuki Kasahara, Kenji Asakawa, Kasumi Nagao, Keita Nakamoto, Kengo Sakasai, Tomo Takeda, Yasutomo Tateishi, Tetsuo Yasuoka, Koichi Yamada Abstract・・・<<read more>>

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>>