JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ECMP02 Subject Category: Competitive Funding PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Shingo Matsuyama smatsu@chofu.jaxa.jp Members: Shingo Matsuyama Abstract In this research, large scale direct numerical simulation of turbulent flow is performed on supercomputer to clarify the role of very small-scale turbulence in the mixing process of fuel and air. We try to clarify the role of fine-scale turbulence by analyzing the data・・・<<read more>>
JAXA Supercomputer System Annual Report April 2016-March 2017 Edited and Published by: Japan Aerospace Exploration Agency 7-44-1 Jindaiji Higashi-machi, Chofu-shi, Tokyo 182-8522 JAPAN URL: http://www.jaxa.jp/ Editorial Office Supercomputer Division, Security and Information Systems Department Editors Team for "JAXA Supercomputer System Annual Report April 2016-March 2017" Editor in Chief: Naoyuki FUJITA Editors: Atsushi FUJINO, Harumi KATSUNO, Kazuhiro KIMOTO, Satoko MIYAGAWA, Suguru OCHIAI, Susumu TAKATSU, Yuusuke TAKEMOTO, Masahiro YOSHIDA (in Alphabetic Order) Date of Issue Web version: October 31, 2017・・・<<read more>>
1．Outline of the system In addition to SORA-MA, JSS2 consists of advanced systems such as SORA-LM, a large-scale memory system, SORA-PP, a pre-post system, SORA-FS, a file system and J-SPACE an archiving system. JSS2 is also designed for energy saving by adoption of a water-cooling system. JSS2 is composed of these well-developed systems and eco-friendly policy. In April 2016, SORA-MA was updated to the peak performance 3.49 PFLOPS and the total memory size 100 TiB. Since then, JSS2 has been・・・<<read more>>
Aviation Acoustic Vibration Simulation of Cavity Flow with Unstructured CFD Code Adbanced Numerical Simulation of Compressible Two-phase Flow of diesel atomization aFJR high efficiency fan technology development aFJR light weight sound absorption liner technology development Air flow distribution control by a fluidic element Aircraft gust alleviation technology Analysis of the flight characteristic of Jet-FTB Basic research for system integration of silent supersonic airplane technologies CFD analysis of wind turbine wake CFD Simulations of Agriculture Spraying from Multi-Rotor Drones Collaborative・・・<<read more>>
Report Number: R16E0043 Responsible Representative: Kiyoshi Kuramoro(Hokkaido University) Contact Information: Youhei Sasaki(uwabami@math.kyoto-u.ac.jp) Members: Youhei Sasaki, Jun Kimura, Kiyoshi Kuramoro Subject Category: Space(Space philosophy) Abstract We will clarify the current internal state of Mercury and the evolution by numerical calculations of the internal structure and the intrinsic magnetic field generation and comparing with the data obtained from observations. Goal Numerical analysis of Mercury's thermal history, evolution of the metallic core, intrinsic magnetic field generation were carried out in consideration of the・・・<<read more>>
