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Numerical Simulations of Fully Developed Turbulence

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EACA05 Subject Category: JSS Inter-University Research PDF Responsible Representative: Susumu Goto, Professor, Osaka University Contact Information: Susumu Goto(s.goto.es@osaka-u.ac.jp) Members: Ryo Araki, Kento Eguchi, Yutaro Fujiki, Jun Fujino, Susumu Goto, Yusuke Koide, Satoshi Matsumoto, Daiki Watanabe Abstract Since fully developed turbulence at high Reynolds numbers plays an important role in many systems of aerospace engineering, its prediction and control are crucial in various projects. We need to employ a turbulence model・・・<<read more>>

high-level data processing of science satellite data

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EDU10503 Subject Category: Space and Astronautical Science PDF Responsible Representative: Ken Ebisawa, Professor, Institute of Space and Astronautical Science Contact Information: Ken Ebisaa (ISAS)(ebisawa.ken@jaxa.jp) Members: Ken Ebisawa, Miki Kurihara, Satoshi Nakahira Abstract Carrying out high-level data processing of a large amount of science satellite data, and promote research in high energy astrophsics Reference URL N/A Reasons and benefits of using JAXA Supercomputer System In high-energy astronomy research using large amounts・・・<<read more>>

Study of high-order unstructured mesh methods for LES around complicated geometries.

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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>>

Fundamental Researches of Fluid and Combustion for the Hypersonic Flight

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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>>

Numerical analysis on atomization and spray combustion

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EA2150 Subject Category: Aeronautical Technology PDF Responsible Representative: Tatsuya Ishii, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub(matsuura.kazuaki@jaxa.jp) Members: Kazuaki Matsuura, Kinya Saito, Jun Iino, Huilai Zhang, Naoki Nakamura, Mitsumasa Makida Abstract A numerical study is performed to clarify phenomena on atomization and spray combustion. Reference URL N/A Reasons and benefits of using JAXA・・・<<read more>>