Report Number: R16E0040 Responsible Representative: Seiji Zenitani(National Astronomical Observatory of Japan, Division of Theoretical Astronomy) Contact Information: Seiji Zenitani(zenitani@rish.kyoto-u.ac.jp) Members: Tsugunobu Nagai, Seiji Zenitani Subject Category: Space(Space science,Space philosophy) Abstract We conduct scientifitc researches on basic processes in space plasma environments, by using numerical simulations. We also develop an open-source simulation code. Goal To conduct a scientific research on basic processes in space plasmas Objective To develop a magnetohydrodynamic (MHD) simulation code for space plasma research References and Links Please・・・<<read more>>
Report Number: R16E0037 Responsible Representative: Yoshikazu Makino(Next Generation Aeronautical Innovation Hub Center, Aeronautical Technology Directorate) Contact Information: Yasutada Tanabe(tan@chofu.jaxa.jp) Members: Masahiko Sugiura, Yasutada Tanabe, Hideaki Sugawara Subject Category: Aviation(Aircraft) Abstract In Fiscal Year 2016, aerodynamic data of a conceptual model that has been flight tested are obtained and used to validate the CFD tool rFlow3D developed for rotorcraft. The aerodynamic interactions between a main rotor and a wing are simulated. Reduction of the downloading on the wing by a trailing・・・<<read more>>
Report Number: R16E0036 Responsible Representative: Takeshi Ito(Aeronautical Technology Directorate, Next Generation Aeronautical Innovation Hub Center) Contact Information: Shigeru Kuchiishi(kuchi-ishi.shigeru@jaxa.jp) Members: Shigeru Kuchiishi, Minoru Yoshimoto, Shinsuke Nishimura, Kei Nakanishi, Yukinori Morita, Takuya Ogura, Kyohei Sawada Subject Category: Aviation(Aircraft) Abstract A Multi-Objective Evolutionary Algorithm (MOEA) is employed as an aerodynamic optimization method and the optimization tool is aimed to enable the direct evolutionary computing to perform within a practical computational time by FaSTAR. In the present project, basic programs are developed and・・・<<read more>>
