@inproceedings{oai:jaxa.repo.nii.ac.jp:00006634,
 author = {浜辺, 正昭 and 児玉, 秀和 and 山脇, るり子 and 山本, 一臣 and 榎本, 俊治 and 山根, 敬 and 野崎, 理 and Hamabe, Masaaki and Kodama, Hidekazu and Yamawaki, Ruriko and Yamamoto, Kazuomi and Enomoto, Shunji and Yamane, Takashi and Nozaki, Osamu},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {Recently, CFD analyses have been actively applied to the development of a lot of components of air breezing engines. Among them an unsteady multi-stage flow analysis, which is able to simulate unsteady flow within blade passages, plays an important role. This paper introduces an analysis of turbine model testing machine for an example of the unsteady stage analysis including complicated geometries by use of UPACS (Unified Platform for Aerospace Computational Simulation, developed by National Aerospace Laboratory) extended to the analysis of unsteady rotor-stator interaction. Comparison with existing unsteady stage analysis solver CAS3DU, some advantages of UPACS are shown., 資料番号: AA0047427033, レポート番号: JAXA-SP-03-002},
 pages = {184--189},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {複雑形状を有するタービン翼列の非定常解析},
 volume = {JAXA-SP-03-002},
 year = {2004}
}