JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2117 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Yamane, Aeronautical Technology Directorate, Propulsion Research Unit Contact Information: Mitsumasa Makida makida.mitsumasa@jaxa.jp Members: Mitsumasa Makida(JAXA), Naoki Nakamura(ASIRI) Abstract In this research, we aim to obtain design methods for development of aircraft combustors with real configuration, which estimate dispersion of the fuel droplets, evaporation, and combustion processes. Reference URL N/A Reasons for using JSS2 It is important to do parametric case study・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2820 Subject Category: Aeronautical Technology PDF Responsible Representative: Kazuomi Yamamoto, FQUROH Project Team, Aeronautical Technology Directorate Contact Information: Kazuomi Yamamoto yamamoto.kazuomi@jaxa.jp Members: Akihisa Shimada, Kazuomi Yamamoto, Yasushi Ito, Mitsuhiro Murayama, Ryotaro Sakai Abstract This collaborative research is being carried out as part of the FQUROH project aimed at raising the technical maturity level of the noise reduction technology for landing gear, which draws international attention to reduce noise in areas・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ECMP01 Subject Category: Competitive Funding PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Atsushi Hashimoto hashimoto.atsushi@jaxa.jp Members: Atsushi Hashimoto, Tsukasa Nagao Abstract We evaluate the hyperbolic equations for Navier-Stokes equations. Reference URL Please refer to 'KAKEN — Research Projects | 双曲型ナビエ・ストークス方程式に基づいた高レイノルズ数遷音速流解析の革新的高速化 (KAKENHI-PROJECT-15K18286)'. Reasons for using JSS2 We plan a large scale computation in the future. Achievements of the Year We studied a laminar flow・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA10 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Shun Takahashi, Tokai University Contact Information: Shun Takahashi takahasi@tokai-u.jp Members: Shun Takahashi Abstract Two-phase flows with moving objects are commonly used in practical engineering products. This study is subject to investigate the effect of the micro particles in the exhausted gas from the rocket engine to the strong pressure waves and the thermal conductance modification due to the water film around・・・<<read more>>
