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Study of combustion instability

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECMP16 Subject Category: Competitive Funding PDF Responsible Representative: Seiji Tsutsumi, Research and Development Directorate, Research Unit III Contact Information: Seiji Tsutsumi(tsutsumi.seiji@jaxa.jp) Members: Junya Aono, Hiroyuki Ito, Noriyasu Omata, Seiji Tsutsumi Abstract In this study, LS-FLOW-HO was used to conduct a two-dimensional LES analysis of Continuously Variable Resonant CoContinuously Variable (CVRC) with varying inlet oxidizer temperature. Then, the database with and without combustion instability was generated. We will develop a reduced・・・<<read more>>

En-Core Project / Turbine aerodynamic performance analysis

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EBA30311 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Ymane, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project Contact Information: Junichi Kazawa, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project(kazawa.junichi@jaxa.jp) Members: Yasuo Horiguchi, Susumu Kato, Junichi Kazawa Abstract We will contribute to strengthening international competitiveness by demonstrating technologies for high-temperature, high-efficiency turbines and ultra-low NOx lean burn combustors that reduce nitrogen oxide (NOx) and・・・<<read more>>

En-Core Project / Turbine internal cooling analysis

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EBA30312 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Ymane, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project Contact Information: Junichi Kazawa, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project(kazawa.junichi@jaxa.jp) Members: Susumu Kato, Junichi Kazawa, Yoji Okita Abstract We will contribute to strengthening international competitiveness by demonstrating technologies for high-temperature, high-efficiency turbines and ultra-low NOx lean burn combustors that reduce nitrogen oxide (NOx) and・・・<<read more>>

Research on the performance improvement of practical aero-engine fuel injector

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EBA30200 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Yamane, Aeronautical Technology Directorate, En-Core Project team Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, En-Core Project team(matsuura.kazuaki@jaxa.jp) Members: Kazuaki Matsuura, Kinya Saito, Takahiro Inagawa, Jun Iino, Kunihiko Sakata, Aya Yoshida, Kodai Kato, Mitsumasa Makida, Naoki Nakamura Abstract Our study is focusing on the improvement of fuel injector performance. Numerical simulations on air-flow, atomization, fuel/air mixing, combustion, and・・・<<read more>>

Numerical analysis on fuel injector design

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EBA30201 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Yamane, Aeronautical Technology Directorate, En-Core Project team Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, En-Core Project team(matsuura.kazuaki@jaxa.jp) Members: Kazuaki Matsuura, Jun Iino, Takahiro Inagawa, Kinya Saito, Aya Yoshida, Kunihiko Sakata Abstract Numerical simulations of thermofluid dynamics are performed to optimize fuel injector design. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System The use of・・・<<read more>>