@inproceedings{oai:jaxa.repo.nii.ac.jp:00003845,
 author = {藤田, 直行 and Fujita, Naoyuki},
 book = {宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県, 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan, JSS(Jaxa Supercomputer System) is the first supercomputer system for Japan Aerospace Exploration Agency(JAXA). On JSS, fruitful numerical simulation have been calculate, for example, launch pad noise analysis, liquid fuel atomization, design of rocket engine, airplane landing gear sound analysis, shock wave on wing, and so on. Five years or more have passed since the system operation start. From that time by the present, aggressive use of numerical simulation on aerospace field is continuing. As a result, supercomputer resource became insufficient. Main requirements are (1) Increase computing power, (2) Correspondence to the analysis of an unsteady phenomenon, (3) Necessity for file system and archive system, (4) Large scale pre/post-processing realization, (5) Realization of the backup function ofexperimental data and/or observational data. So JAXA decided to replace supercomputer system. This shows a purpose of the installation and JSS generation 2 composition outlines., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530023010, レポート番号: JAXA-SP-14-010},
 pages = {53--56},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {JAXA新スパコンJSS2の導入目的と構成概要},
 volume = {JAXA-SP-14-010},
 year = {2015}
}