@inproceedings{oai:jaxa.repo.nii.ac.jp:00038243,
 author = {山根, 敬 and 榎本, 俊治 and 高木, 亮治 and 山本, 一臣 and Yamane, Takashi and Enomoto, Shunji and Takaki, Ryoji and Yamamoto, Kazuomi},
 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2002論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002},
 month = {Mar},
 note = {UPACS, Unified Platform for Aerospace Computational Simulation, is a project to develop a common CFD platform since 1998 at National Aerospace Laboratory of Japan. The project aims not only to overcome the increasing difficulty in recent CFD code programming on parallel computers for aerospace applications, but also to accelerate the development of CFD technology by sharing a common base code among research scientists and engineers. The first version of the UPACS has been released in 2000 with the capability to solve compressible flows using the multi-block structured grid method and it has become to be able to treat overset grids and solve rotating cascade flows. The UPACS is being extended toward multidisciplinary problems such as the coupling of flow simulation with heat conduction and the simultaneous calculations of flow around turbine blade and heat conduction inside blade material has become possible., 資料番号: AA0045948022, レポート番号: NAL SP-57},
 pages = {124--129},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {UPACSによる流体・熱伝導連成解析について},
 volume = {57},
 year = {2003}
}