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Development of 3D CFD core-software of automotive engine combustion chamber

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201N11 Subject Category: Aeronautical Technology PDF Responsible Representative: MizobuchiYasuhiro, Director, Aviation Technology Directrate, Aviation Lifecycle Innovation Hub Contact Information: Taisuke Nambu, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub(nambu.taisuke@jaxa.jp) Members: Hiroyuki Abe, Atsusi Fujino, Manabu Hisida, Takaaki Kishi, Ryohei Kirihara, Takuhito Kuwabara, Daiki Miyai, Yasuhiro Mizobuchi, Taisuke Nambu, Daichi Obinata, Kei Shimura, Shogo Yasuda, Hiroki Yao Abstract Enhancement of CAE utilization in automotive engine research by developing an engine combustion simulation・・・<<read more>>

Numerical analysis for optimal design of helicopter rotor blades

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201C22 Subject Category: Aeronautical Technology PDF Responsible Representative: Hitoshi Arizono,Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Aeronautical Technology Directorate Contact Information: Keita Kimura(kimura.keita@jaxa.jp) Members: Fumihiro Kajiwara, Keita Kimura, Masahiko Sugiura, Hideaki Sugawara, Yasutada Tanabe Abstract A cooperative study of rotor blade optimization methods is being conducted by JAXA, DLR, and ONERA to validate rotor blade analysis tools and optimization methods, and to accumulate knowledge. In this fiscal year, optimization・・・<<read more>>

Development of Aeroelastic Simulation Tool based on FaSTAR-Move

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G02 Subject Category: Aeronautical Technology PDF Responsible Representative: Hitoshi Arizono, Aircraft Lifecycle Innovation Hub Contact Information: Hitoshi Arizono(arizono.hitoshi@jaxa.jp) Members: Hitoshi Arizono, Kohei Konishi, Hamidreza Kheirandish Abstract Development of Aeroelastic Simulation Tool based on FaSTAR-Move Reference URL N/A Reasons and benefits of using JAXA Supercomputer System Aeroelastic analysis requires unsteady analysis. Therefore, it is necessary to use JSS2 because the simulation cost is high. Achievements of the Year Inplemented the moving・・・<<read more>>

High-Reynolds number stall characteristics of a wing-body configuration model

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G10 Subject Category: Aeronautical Technology PDF Responsible Representative: Kazuyuki Nakakita, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Kazuyuki Nakakita, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub(nakakita.kazuyuki@jaxa.jp) Members: Kuniyuki Takekawa, Takahiro Yamamoto Abstract Aerodynamic characteristics of a fundamental wing-body configuration model was analyzed by CFD to compare with High-Reynolds number wind tunnel data conducted in JAXA’s collabollation research. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>

Research on Particle Simulation Methods

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EDA201G19 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aviation Technology Directorate, Program Director Contact Information: Kenichi Kubota, Aircraft Lifecycle Innovation Hub, Aviatoin Technology Directorate(kubota.kenichi@jaxa.jp) Members: Kenichi Kubota, Keita Nakamoto Abstract The purpose of this research is to obtain the simulation technology of particle simulation, known to be useful for analysing multi-physics phenomena, to accelerate aircraft development. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System JSS3・・・<<read more>>