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Numerical Study on Combustible Flow in Supersonic Flight Engines and Rocket Engines

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA01 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Nobuyuki Tsuboi, Department of Mechanical and Control Engineering, Kyushu Institute of Technology Contact Information: Nobuyuki Tsuboi tsuboi@mech.kyutech.ac.jp Members: Satoshi Koduka, Maiko Iwai, Toshihiro Iwasa, Takahide Araki, Keisuke Yoshida, Nobuyuki Tsuboi, Yoshiki Nishikawa, Tomoki Uzaki, Ryuji Takahashi, Ayu Agou, Kouhei Ozawa, Hichamnicolas Jourdaine Abstract Fundamental studies on nozzles and combustors for Japanese rocket engines and supersonic engines are performed by using numerical・・・<<read more>>

Requirement analysis for LiteBIRD's optical system

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA34 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Ryo Nagata, High Energy Accelerator Research Organization (KEK) Contact Information: Ryo Nagata rnagata@post.kek.jp Members: Ryo Nagata Abstract Primordial gravitational wave background is generically predicted by cosmic inflation theories. Its amplitude indicates the energy scale of cosmic inflation. LiteBIRD maps the polarization of microwave background sky to detect the signal of the gravitational waves. Since the signal of gravitational wave origin (B-mode・・・<<read more>>

Numerical study of the convection structure in Venus' atmospheres

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA14 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Ko-ichiro Sugiyama, National Institute of Technology, Matsue College Contact Information: Ko-ichiro Sugiyama sugiyama@gfd-dennou.org Members: Ko-ichiro Sugiyama, Hiroki Ando Abstract Our purpose is to support the observation performed by AKATSUKI (Venus Climate Orbiter) by developing a numerical fluid dynamics model (cloud resolving model) and providing a lot of numerical simulation data. The motion of Venus' cloud-level convection and the propagation of gravity・・・<<read more>>

Numerical Study of Breakdown and Shock Wave Structures for Improvement of Flight Performance in a Beamed-Energy Vehicle

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA17 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Masayuki Takahashi, Tohoku University Contact Information: Masayuki Takahashi mtakahashi@rhd.mech.tohoku.ac.jp Members: Masayuki Takahashi Abstract Propulsion performance of a beamed-energy vehicle is improved by reproducing breakdown physics and shock wave propagation induced inside a rocket nozzle. Reference URL N/A Reasons for using JSS2 We used JSS2 because computational costs for reproducing a multi-dimensional physics of the breakdown process and shock wave propagation inside・・・<<read more>>

Numerical Analysis of Low-Speed Buffet using High-Resolution Scheme

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA1935 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi AOYAMA, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Atsushi Hashimoto hashimoto.atsushi@jaxa.jp Members: Takuya Aogaki, Atsushi Hashimoto, Keiichi Kitamura, Kanta Fukumoto, Ayano Inatomi, Toshiaki Harada, Suguru Ogawa, Yuuya Takagi, Hiroyuki Takimoto, Hiroto Yaginuma Abstract Post Limiter has been improved to "Post Limiter 3(new)", and incorporated into JAXA's flow analysis code "FaSTAR." Then, its performance has been demonstrated in several aerodynamic・・・<<read more>>