本文へ移動

サイトナビゲーションへ移動

検索ボックスへ移動

サイドバーへ移動

ここは、本文エリアの先頭です。

Research of unsteady flow simulation toward prediction of full flight envelope

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA201N01 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Atsushi Hashimoto, Aeronautical Technology Directorate, Numerical Simulation Research Unit(hashimoto.atsushi@jaxa.jp) Members: Takashi Ishida, Atsushi Hashimoto, Kenji Hayashi, Takashi Aoyama, Takahiro Yamamoto, Masashi Kanamori, Yuki Ide, Hideaki Aiso, Keita Nakamoto, Andrea Sansica, Tomoaki Matsuzaki, Paul Zehner, Hisato Takeda, Yoimi Kojima, Yuuki Asada, Kanako Yasue, Ryosuke Fuse, Kei Shimura, Ryohei Kirihara, Manabu Hishida Abstract・・・<<read more>>

Flight Demonstration of Gust Alleviation Technologies

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA102H00 Subject Category: Aeronautical Technology PDF Responsible Representative: Atsushi Kanda, Hub Manager, Aeronaitical Technology Directorate, Next Generation Aeronautical Innovation Hub Center, WEATHER-Eye Team Contact Information: Midori Maki, Aeronaitical Technology Directorate, Next Generation Aeronautical Innovation Hub Center, WEATHER-Eye Team(maki.midori@jaxa.jp) Members: Manabu Hishida Abstract Flight demonstration of gust alleviation control technologies using JAXA doppler lidar Reference URL N/A Reasons and benefits of using JAXA Supercomputer System Database construction of aerodynamics of a・・・<<read more>>

Nonlinear Aeroelastic Framework for Multi-fidelity Analysis

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA101S01 Subject Category: Aeronautical Technology PDF Responsible Representative: Hitoshi Arizono, Aeronautical Technology Directorate, Structures and Advanced Composite Research Unit Contact Information: Hitoshi Arizono(arizono.hitoshi@jaxa.jp) Members: Hitoshi Arizono, Youichi Sano, Natsuki Tsushima Abstract Nonlinear Aeroelastic Framework for Multi-fidelity Analysis Reference URL N/A Reasons and benefits of using JAXA Supercomputer System Because high fidelity analysis is very expensive for simulation Achievements of the Year An unsteady vortex-lattice aerodynamic method and a fast unstructured・・・<<read more>>

Research on Techniques of Sound Absorbing Liner Analysis

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA101P01 Subject Category: Aeronautical Technology PDF Responsible Representative: Tatsuya Ishii, Aeronautical Technology Directorate, Propulsion Research Unit Contact Information: Nobuhiko Yamasaki, Department of Aeronautics and Astronautics, Kyushu University(yamasaki@aero.kyushu-u.ac.jp) Members: Soufiane Ramdani, Genki Omagari, Nobuhiko Yamasaki (Kyushu University), Kenichiro Nagai, Tatsuya Ishii Abstract The technique to analyze the sound absorbing lines with bias flows, the air flow through porous plate, is to be established and used for the clarification of the physics・・・<<read more>>

Fundamental Research on Noise Generation Mechanisms from Airframe

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19ECWU02 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Kazuomi Yamamoto, FQUROH+ Team, Aviation Systems Research Unit, Aeronautical Technology Directorate Contact Information: Kazuomi Yamamoto(yamamoto.kazuomi@jaxa.jp) Members: Yutaku Yan, Kazuomi Yamamoto, Mitsuhiro Murayama, Yasushi Ito, Takehisa Takaishi, Ryotaro Sakai, Tohru Hirai, Kentaro Tanaka, Kazuhisa Amemiya, Gen Nakano Abstract The noise reduction technology for high-lift devices and landing gear draws international attention to reduce noise in areas around airports. FQUROH (Flight Demonstration・・・<<read more>>