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Numerical analysis on atomization and spray combustion

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA2150 Subject Category: Aeronautical Technology PDF Responsible Representative: Tatsuya Ishii, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub(matsuura.kazuaki@jaxa.jp) Members: Kazuaki Matsuura, Kinya Saito, Jun Iino, Naoki Nakamura, Mitsumasa Makida Abstract A numerical study is performed to clarify phenomena on atomization and spray combustion. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>

Research on Structure and Composite Material Technologies for Digital Certification

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA1601 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: Yuichiro Aoki, Yoshiyasu Hirano, Kenichi Kubota, Shintaro Kamiyama, Toshiyuki Kasahara, Hiroki Kawabe, Kasumi Nagao, Keita Nakamoto, Yasutomo Tateishi, Tetsuo Yasuoka Abstract The objective of this research is to accurately model manufacturing defects in・・・<<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 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>>