@inproceedings{oai:jaxa.repo.nii.ac.jp:00038050,
 author = {向井, 純一 and 山本, 一臣 and 山根, 敬 and 野崎, 理 and Mukai, Junichi and Yamamoto, Kazuomi and Yamane, Takashi and Nozaki, Osamu},
 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 common CFD platform program developed at National Aerospace Laboratory. The project to develop UPACS aims not only to overcome the increasing difficulty in recent CFD code programming on parallel computers, but also to accelerate the development of CFD technology by sharing a common base code among research scientists and engineers. This paper reports the extension to a rotary coordinate system of UPACS and computational results of the flow around transonic compressor rotors, NASA rotor 37 and rotor 35, which have the number of published computational and experimental works., 資料番号: AA0032819014, レポート番号: NAL SP-53},
 pages = {81--86},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {UPACSによるエンジン内部流れの計算},
 volume = {53},
 year = {2002}
}