[Added on] Apr 16, 2021 [Last modified on] Dec 7, 2021

JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDG20201 Subject Category: Research and Development PDF Responsible Representative: Chofuku Shintaro, Reserch InsertHere Development Directorate, Unit 4 Contact Information: Chofuku Shintaro(chofuku.shintaro@jaxa.jp) Members: Shintaro Chofuku Abstract Research and study topology optimization and verify its applicability to spacecraft. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System For network license. Achievements of the Year N/A Publications N/A Usage of JSS Computational Information Process Parallelization Methods: N/A Thread Parallelization Methods: N/A・・・<<read more>>

[Added on] Apr 16, 2021 [Last modified on] Dec 7, 2021

JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDG20200 Subject Category: Research and Development PDF Responsible Representative: KIMURA Toshiyoshi, Director, Sensor System Research Group, Research and Development Directorate Contact Information: Rei Mitsuhashi, Yoshito Sawada(mitsuhashi.rei@jaxa.jp) Members: Rei Mitsuhashi, Yoshito Sawada Abstract For the ISS LIDAR mission (MOLI:Multi-footprint Observation Lidar and Imager), we are considering the specified Project Use of JSS3 for the ground processing system due to the characteristics of MOLI project. In this project, we will study the・・・<<read more>>

[Added on] Apr 16, 2021 [Last modified on] Dec 7, 2021

JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201P73 Subject Category: Aeronautical Technology PDF Responsible Representative: Keiichi OKAI, Assoiciate Senior Researcher, Aeronautical Technology Directorate, Aeroengine Technology Demonstration Section Contact Information: Keiichi OKAI(okai.keiichi@jaxa.jp) Members: Keiichi Okai, Junichi Kazawa, Akiyoshi Masaki Abstract In this study, evaluation of unsteady aerodynamics in aircraft fan under strongly distorted inflow condition simulating airframe/engine integration configuration with Boundary Layer Ingestion (BLI) benefit suited for future electric aircraft. Under these BLI conditions, aircraft fan suffers almost・・・<<read more>>

[Added on] Apr 16, 2021 [Last modified on] Dec 7, 2021

JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201N11 Subject Category: Aeronautical Technology PDF Responsible Representative: MIZOBUCHI Yasuhiro, Senior researcher, Aeronautical echnology Directrate, Numerical Simulation Research Unit Contact Information: MIZOBUCHI Yasuhiro, Japan Aerospace Exploration Agency, Aeronautical Technology Directrate(mizo@chofu.jaxa.jp) Members: Taisuke Nambu, Hiroki Yao, Shogo Yasuda, Yasuhiro Mizobuchi, Hiroyuki Abe, Manabu Hisida, Atsusi Fujino, Daichi Obinata, Takuhito Kuwabara, Shintaro Koike, Mikiroh Motoe, Kei Shimura, Toshikuni Koganei Abstract Enhancement of CAE utilization in automotive engine research by developing an engine・・・<<read more>>

[Added on] Apr 16, 2021 [Last modified on] Dec 7, 2021

JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201N10 Subject Category: Aeronautical Technology PDF Responsible Representative: Keiichi Kitamura, Yokohama National University, Faculty of Engineering, Division of Systems Research Contact Information: Keiichi Kitamura(kitamura@ynu.ac.jp) Members: Atsushi Hashimoto, Keiichi Kitamura, Masashi Kanamori, Hayato Kawashima, Yoshikatsu Furusawa, Takuma Yamaguchi, Fumiya Tsutsui, Yuya Yasumura, Tomohiro Mamashita, Kazuki Kakizaki, Shogo Motoki, Kiyokaze Okayama, Hirokazu Kurihara, Kaede Makino, Daichi Ishdo Abstract A high-resolution, Delayed DES has been conducted around whole the aircraft under the low-speed・・・<<read more>>