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.
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>>
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>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA20 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Keiichi Kitamura, Yokohama National University Contact Information: Toshiaki Harada harada-toshiaki-vt@ynu.jp Members: Toshiaki Harada, Keiichi Kitamura Abstract It is important for rocket developments to quantitatively estimate the influence of protuberances in the flight vehicles which create asymmetry of flow around the vehicles and aerodynamic forces. Using fluid numerical computation, it is expected that we obtain a guideline for the protuberance choice in・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA3301 Subject Category: Aeronautical Technology PDF Responsible Representative: Yasutada Tanabe, Aeronautical Technology Directorate, Next Generation Aeronautical Innovation Hub Center Contact Information: Yasutada Tanabe tanabe.yasutada@jaxa.jp Members: Masahiko Sugiura, Yasutada Tanabe, Hideaki Sugawara, Ryo Hayakawa Abstract A distinctive concept of compound helicopter is proposed by JAXA. Several key technologies have been recognized and investigated so far. Within them, the aerodynamic interaction between the main rotor and the wing may cause remarkable increase・・・<<read more>>
