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Numerical analysis of deicing and anti-icing in jet engine

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA101H11 Subject Category: Aeronautical Technology PDF Responsible Representative: Atsushi Kanda, Aviation Technology Directorate, Aviation Safety Innovation Hub Contact Information: Junichi Kazawa, Aviation Technology Directorate, Aviation Safety Innovation Hub(kazawa.junichi@jaxa.jp) Members: Yasuo Horiguchi, Junichi Kazawa, Masaya Suzuki Abstract Technology development is conducted to solve the icing problem in jet engines. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System To perform large-scale analysis. Achievements of the Year We conducted a・・・<<read more>>

Acoustic Liner Program for High-bypass-ratio Aircraft engines (acoustic performance improvement)

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA101C75 Subject Category: Aeronautical Technology PDF Responsible Representative: Kenichiro Nagai, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: Shunji ENOMOTO(enomoto.shunji@jaxa.jp) Members: Shunji Enomoto, Kenichiro Nagai, Hideshi Oinuma, Junichi Oki, Gai Kubo, Tatsuya Ishii Abstract Ultra high bypass ratio aviation jet engines have a smaller sound absorbing liner area than conventional engines. In this project, we will develop sound-absorbing device technology that provides high noise reduction performance even with・・・<<read more>>

Acoustic Liner Program for future High-bypass-ratio Aircraft engines(Development of combustor)

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA101C39 Subject Category: Aeronautical Technology PDF Responsible Representative: Kenichiro Nagai, Aeronautical Technology Directorate,Aviation Environmental Sustainability Innovation Contact Information: Naoyuki Okamura(okamura.naoyuki@jaxa.jp) Members: Taisuke Nambu, Hideji Saiki Abstract In this project, we will apply next-generation acoustic liner to combustor. To perform the numerical analysis of combustor with the acoustic liner by using HINOCA-AE which is CFD solver for aircraft engine combustors. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>

Development of a high-precision unstructured mesh flow solver for aerodynamic design of turbomachinery cascade

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA101C13 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: Manabu Hisida, Hamidreza Kheirandish, Junichi Kazawa, Takahisa Kohno, Taisuke Nambu, Kanako Yasue Abstract FaSTAR-Move-AE, a fluid analysis solver for unstructured meshes, which is mainly targeted at turbomachinery analysis, is developed. This solver will enable aerodynamic analysis of cascades・・・<<read more>>

Gas-Liquid Two Phase Flow Behavior Related to ECLSS

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23ECWU77 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Masato Sakurai, Manager for ECLSS Contact Information: Masato Sakurai(sakurai.masato@jaxa.jp) Members: Motoharu Kusano, Gaku Murakami, Masato Sakurai Abstract Elucidate the effects of gravity on gas-liquid two-phase flows to develop separation techniques for gas-liquid two-phase flows generated by the operation of the Environment Control and Life Support System (ECLSS). Reference URL N/A Reasons and benefits of using JAXA Supercomputer System In order・・・<<read more>>