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

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA2120 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: Kenji Hayashi, Junichi Kazawa, Takahisa Kohno, Taisuke Nambu, Hiroki Ugajin, Kanako Yasue Abstract Unstructured-grid flow solver FaSTAR-Move-AE are applied to aero-engine analysis with complicated configuration. Through the calculation, these programs are tested and investigated for the deficiency and・・・<<read more>>

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

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA0714 Subject Category: Aeronautical Technology PDF Responsible Representative: Mitsumasa Makida(JAXA, Aeronautical Technology Directorate) Contact Information: Mitsumasa Makida(Aeronautical Technology Directorate)(makida.mitsumasa@jaxa.jp) Members: Mitsumasa Makida, Naoki Nakamura, Takashi Ishiyama Abstract In the development process of aircraft combustors, air mass flow distribution between fuel nozzles and cooling air holes on the liner effects performances of combustors. In this research, we conduct combustion simulations of internal flow inside the combustor which faithfully simulates the configuration・・・<<read more>>

Aerodynamic testing technology for reentering capsules

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA1403 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>>

Research of laminar fin system

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA0601 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: Hitoshi Arizono, Takahiro Ishida, Shunsuke Imai, Fumitake Kuroda, Keisuke Ohira, Satoshi Kondo, Dongyoun Kwak, Takashi Matsuno, Tatsuya Nishimoto, Shota Yamamoto, Naoko Tokugawa, Keiji Ueshima, Hayahide Yoshida Abstract The laminar flow vertical tail fins are designed and evaluated to establish practical technology for a natural laminar flow・・・<<read more>>

Research on Aircraft Multidisciplinary Design Technology

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA0602 Subject Category: Aeronautical Technology PDF Responsible Representative: Dongyoun Kwak, Aviation Technology Directorate, Aviation Enviromental Sustanability Innovation Hub Contact Information: Mitsuhiro Murayama, Aviation Technology Directorate, Aviation Environmental Sustainability Innovation Hub(murayama.mitsuhiro@jaxa.jp) Members: Ryutaro Furuya, Tohru Hirai, Tomoaki Ikeda, Yasushi Ito, Fumitake Kuroda, Keisuke Ohira, Junichi Kazawa, Dongyoun Kwak, Mitsuhiro Murayama, Kentaro Tanaka, Kuniyuki Takekawa Abstract The purpose of the research is to develop and mature a bunch of advanced and innovative・・・<<read more>>