@inproceedings{oai:jaxa.repo.nii.ac.jp:00003631,
 author = {藤田, 直行 and Fujita, Naoyuki},
 book = {宇宙航空研究開発機構特別資料: 第47回流体力学講演会/第33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 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京, 47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro, Tokyo, Japan, JAXA Supercomputer System generation 2 (JSS2) has begun to work from October 1, 2014. When we think back to history of a supercomputer of JAXA, FACOM-230-75APU promotes a CFD study, FACOM VP400 makes a practical use of RANS equation simulation, Numerical Wind Tunnel (NWT) realized parametric study using steady flow simulation. By JSS2, we are going to do unsteady flow parametric study, data processing which is new comer for JAXA supercomputer system, and so on. JSS2 consists of computing facility named SORA (Supercomputer for earth Observation, Rockets, and Aeronautics) and archival system named J-SPACE (Jaxa's Storage Platform for Archiving, Computing, and Exploring)., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630005006, レポート番号: JAXA-SP-15-013},
 pages = {47--52},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {JSS2システム概要と活用・運用},
 volume = {JAXA-SP-15-013},
 year = {2016}
}