@inproceedings{oai:jaxa.repo.nii.ac.jp:00038067,
 author = {中尾, 雅弘 and Nakao, Masahiro},
 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 = {In this paper, an analysis method for predicting flowfield around a helicopter using a 3D Cartesian grid is presented. This system simplifies a grid generation and is applied easily to a flowfiled including multiple boundaries. The system consists of an Euler solver using AUSM-DV scheme. Applications to flowfields around the NACA0012 airfoil are done and comparison between numerical results and experimental data show good agreement. Also, flowfields around a full configuration helicopter are calculated. The results show the capability of the code and present useful information at the stage of conceptual design., 資料番号: AA0032819031, レポート番号: NAL SP-53},
 pages = {179--184},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {直交格子を用いたヘリコプタ全機流れ場解析},
 volume = {53},
 year = {2002}
}