@inproceedings{oai:jaxa.repo.nii.ac.jp:00038051,
 author = {高木, 亮治 and 石川, 敬掲 and 岩宮, 敏幸 and Takaki, Ryoji and Ishikawa, Hiroaki and Iwamiya, Toshiyuki},
 book = {航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001},
 month = {Jan},
 note = {UPACS, Unified Platform for Aerospace Computational Simulation, is a project to develop a common CFD platform since 1998 at National Aerospace Laboratory. UPACS solver version 1.0 was released on Oct. 2 2000. This paper presents several applications of UPACS, especially for external flow analysis. First application is stall prediction of 2D airfoil, showing the effects of an artificial transition model. Another is supersonic flow analysis around NEXST-1 (National EXperimental Supersonic Transport-1), which is scheduled to conduct flight experiment in 2002, showing a grid dependency for friction drag It is important to accumulate these application results in order to enhance reliability of UPACS., 資料番号: AA0032819015, レポート番号: NAL SP-53},
 pages = {87--92},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {UPACSによる航空機まわりの流れの計算},
 volume = {53},
 year = {2002}
}