JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24EEG70101 Subject Category: Research and Development PDF Responsible Representative: Yudai Konno Research Unit 4 Research and Development Directorate Contact Information: Yudai Konno(konno.yuudai@jaxa.jp) Members: Yudai Konno Abstract Consideration of test facilities for the Public-Private Collaboration Center Reference URL N/A Reasons and benefits of using JAXA Supercomputer System ISV software use only Achievements of the Year Visualization of rocket engine combustion gas flow using STAR CCM+ Publications N/A Usage of JSS Computational・・・<<read more>>
JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24EA0714 Subject Category: Aeronautical Technology PDF Responsible Representative: Mitsumasa Makida(JAXA, Aeronautical Technology Directorate) Contact Information: Mitsumasa Makida(JAXA, Aeronautical Technology Directorate)(makida.mitsumasa@jaxa.jp) Members: Takashi Ishiyama, Mitsumasa Makida, Naoki Nakamura Abstract In the development process of aircraft combustors, air mass flow distribution between fuel nozzles, dilution and cooling air holes on the liner effects performances of combustors. So it is important to understand the internal flow and estimate the mass flow distribution. In・・・<<read more>>
JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24EA1601 Subject Category: Aeronautical Technology PDF Responsible Representative: Tomo Takeda, Aviation Technology Directorate, Aircraft Digital Transformation Technology Demonstration Project Team Contact Information: Tomo Takeda(takeda.tomo@jaxa.jp) Members: Yasutomo Tateishi, Hikaru Hoshi, Yuichiro Aoki, Sunao Sugimoto, Toshiya Nakamura Abstract The objective of this research is to develop a simplified finite element modeling methodology to predict the thermal deformation of carbon fiber reinforced polymer (CFRP) laminates during their automated fiber placement (AFP) manufacturing process.・・・<<read more>>
