@inproceedings{oai:jaxa.repo.nii.ac.jp:00038266,
 author = {畑中, 圭太 and 中村, 佳朗 and Hatanaka, Keita and Nakamura, Yoshiaki},
 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 = {Recently CFD is commonly used in design, where high efficiency is required. The cartesian grid has an advantage over other grids because it is easy to generate grid. However, many grid cells are necessary to correctly capture various flow phenomena, which spoils the merit of the cartesian grid. In the present study, an LU-SGS method is employed for time integration to overcome this problem., 資料番号: AA0045948045, レポート番号: NAL SP-57},
 pages = {253--256},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {次世代超音速旅客機周りの非粘性圧縮流体解析におけるLU-SGS法の検証},
 volume = {57},
 year = {2003}
}