JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2751 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshio Nishizawa, Aeronautical Technology Directorate, aFJR project team Contact Information: Masahiro Hojo hojo.masahiro@jaxa.jp Members: Kenshirou Kondou, Shota Sadamoto, Masahiro Hojo, Takuya Ando, Tomoaki Watanabe, Koji Miyazaki Abstract The purpose of aFJR project is to advance research on jet engine component technologies so that Japanese manufacturers can join more effectively in international joint-development projects on next-generation jet engines. Application of a Ceramic Matrix・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA31 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Soshi Kawai, Department of Aerospace Enginerring, Tohoku University Contact Information: Kosuke Totani totani@cfd.mech.tohoku.ac.jp Members: Soshi Kawai, Kosuke Totani Abstract The aim of this study is to numerically investigate the physics of compressible thermal turbulent boundary layer, and direct numerical simulations (DNS) are performed. The understanding from the DNS analysis will be utilized for building a wall model of large-eddy simulation for・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA13 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Kazuo Matsuura, Ehime University, Graduate School of Science and Engineering Contact Information: Kazuo Matsuura matsuura.kazuo.mm@ehime-u.ac.jp Members: Kazuo Matsuura Abstract In hypersonic transitional flows, there are many complicated factors such as density fluctuation and temperature fluctuation due to the co-existence of the region slower than the speed of sound and the region faster than the speed of sound inside the boundary layer.・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2720 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshio Nishizawa, Aeronautical Technology Directorate, aFJR project team Contact Information: Masahiro Hojo hojo.masahiro@jaxa.jp Members: Masahiro Hojo, Kenshirou Kondou, Shota Sadamoto, Tomoaki Watanabe, Takuya Ando, Koji Miyazaki Abstract The purpose of aFJR project is to advance research on jet engine component technologies so that Japanese manufacturers can join more effectively in international joint-development projects on next-generation jet engines. The technology of the weight・・・<<read more>>
