[Added on] Jul 2, 2018 [Last modified on] Dec 9, 2019

JAXA Supercomputer System Annual Report April 2017-March 2018 JAXA Supercomputer System Annual Report April 2017-March 2018 Edited and Published by: Japan Aerospace Exploration Agency 7-44-1 Jindaiji Higashi-machi, Chofu-shi, Tokyo 182-8522 JAPAN URL: http://www.jaxa.jp/   Editorial Office Supercomputer Division, Security and Information Systems Department Editors Team for "JAXA Supercomputer System Annual Report April 2017-March 2018" Editor in Chief: Naoyuki FUJITA Editors: Atsushi FUJINO, Harumi KATSUNO, Kazuhiro KIMOTO, Satoko MIYAGAWA, Suguru OCHIAI, Susumu TAKATSU, Yuusuke TAKEMOTO (in Alphabetic Order)   Date of・・・<<read more>>

[Added on] Jul 2, 2018 [Last modified on] Oct 3, 2024

Languages of the Report Japanese version is available here at this link, JAXA スーパーコンピュータシステム利用成果報告 (2017年4月～2018年3月) . Access to English Version English version could be accessed with the following links. Web Edition PDF Edition Table of Contents page is located with the link at "JAXA Supercomputer System Annual Report April 2016-March 2017 Contents".   Access to Older/Newer Reports Annual reports of older/newer year are available at this link, JAXA Supercomputer System Annual Report.

[Added on] Jun 11, 2018 [Last modified on] Sep 26, 2018

JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA1901 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Atsushi Hashimoto hashimoto.atsushi@jaxa.jp Members: Takashi Ishida, Atsushi Hashimoto, Kenji Hayashi, Takashi Aoyama, Takahiro Yamamoto, Masashi Kanamori Abstract The objective of this study is to realize CFD that can be used in the entire flight envelope by investigating precise CFD technologies that can be applied to unsteady phenomena, such as aerodynamic buffeting・・・<<read more>>

[Added on] Jun 11, 2018 [Last modified on] Sep 26, 2018

JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA18 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Seiichiro Morizawa,Tottori university Contact Information: Seiichiro Morizawa morizawa@mech.tottori-u.ac.jp Members: Seiichiro Morizawa Abstract The discussion on the aerodynamic characteristcs for a Mars exploration airplane is conducted. The conditon of the airplane is the low Reynolds number and high high Mach number conditions, and the data for conventional airplanes on Earth cannot be direcrely applied to the design of a Mars airplane. So,・・・<<read more>>