JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EACA38 Subject Category: JSS Inter-University Research PDF Responsible Representative: Hiroyuki Asada, Depatment of Aerospace Engineering, Tohoku University Contact Information: Hiroyuki Asada(h.asada@tohoku.ac.jp) Members: Hiroyuki Asada, Keigo Miyazaki Abstract The main objective of this study is to develop a solver based on the discontinuous Galerkin (DG) method to realize high-fidelity large-eddy simulation (LES) of high Reynolds number flows around complicated geometries Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>
JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21ECMP18 Subject Category: Competitive Funding PDF Responsible Representative: Kouichi Okita, Director, Research Unit IV, Research and Development Directorate Contact Information: Masahiro Takahashi(takahashi.masahiro@jaxa.jp) Members: Masaaki Fukui, Susumu Hasegawa, Taku Inoue, Masatoshi Kodera, Toshihiko Munakata, Masaharu Takahashi, Sadatake Tomioka, Masahiro Takahashi, Gouji Yamada Abstract The wind tunnel tests by using sub-scaled models play important roles for the development of the air-breathing propulsion system for a hypersonic transporter. However, in some cases, the・・・<<read more>>
JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EA3201 Subject Category: Aeronautical Technology PDF Responsible Representative: Kanako Yasue, Aviationl Techonology Directorate Contact Information: Kanako Yasue(yasue.kanako@jaxa.jp) Members: Hitoshi Arizono, Atsushi Hashimoto, Kenji Hayashi, Takashi Ishida, Masatoshi Kanayama, Takahisa Kohno, Taisuke Nambu, Kanako Yasue Abstract FaSTAR-Move, an extended version of the fast unstructured-grid flow solver FaSTAR, is developed to analyse flow field around moving/deforming objects such as external store separation, flutter, rotor, and compressor/turbine of aero-engines. Reference URL N/A Reasons・・・<<read more>>
