JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA2150 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshio Nishizawa, Aeronautical Technology Directorate, Propulsion Research Unit Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Propulsion Research Unit(matsuura.kazuaki@jaxa.jp) Members: Kazuaki Matsuura, Naoki Nakamura, Mitsumasa Makida, Huilai Zhang, Jun Iino, Kinya Saito Abstract A numerical study is performed to clarify phenomena on atomization and spray combustion. Reference URL N/A Reasons for using JSS2 In order to analyze a complicated・・・<<read more>>
JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA1601 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshiya Nakamura, Aeronautical Directorate, Structure and Advanced Composite Technology Reasearch Unit Contact Information: Yuichiro Aoki(aoki.yuichiro@jaxa.jp) Members: Akinori Yoshimura, Masaya Ebina, Yuichiro Aoki, Toshiyuki Kasahara Abstract Application of the composite materials will contribute to improving the performance of aircraft and spacecraft components. JAXA conducts researches for overcoming weaknesses of current composite materials, clarifying unknown aspects such as fracture mechanisms, improving performance and enabling・・・<<read more>>
JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA1403 Subject Category: Aeronautical Technology PDF Responsible Representative: Shigeru Hamamoto, Aeronautical Technology Directorate, Aerodynamics Research Unit Contact Information: Hajime Miki(miki.hajime@jaxa.jp) Members: Hajime Miki, Yoshiki Takama Abstract In some cases, a lifting reentry capsule does not have enough attitude control ability. The purpose of this study is to utilize RCS interaction as an auxillary control force by local modification of capsule's external shape. Reference URL N/A Reasons for using JSS2 The・・・<<read more>>
JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA1402 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Ozawa, Research and Development Directorate, Research Unit II Contact Information: Takashi Ozawa(takashi@chofu.jaxa.jp) Members: Toshiyuki Suzuki, Takashi Ozawa, Ryotaro Murakami Abstract To obtain aerothermodynamic data of Mars aerocapture. Reference URL N/A Reasons for using JSS2 It is necessary to use JONATHAN. Achievements of the Year Heat flux distribution around aeroshell was obtained by JONATHAN. As a result, heat flux at stagnation point・・・<<read more>>
