@article{oai:jaxa.repo.nii.ac.jp:00022619,
 author = {橋本, 敦 and 村上, 桂一 and 青山, 剛史 and 菱田, 学 and 坂下, 雅秀 and ラフール, パウルス and Hashimoto, Atsushi and Murakami, Keiichi and Aoyama, Takashi and Hishida, Manabu and Sakashita, Masahide and Lahur, Paulus},
 issue = {3},
 journal = {日本航空宇宙学会論文集, Journal of the Japan Society for Aeronautical and Space Sciences},
 month = {Jun},
 note = {Although CFD tools are necessary for aerodynamic design, it is still time consuming and this is one of the big problems. In order to shorten the computational time, a fast CFD code “FaSTAR” has been developed. We combined two acceleration techniques. One is a convergence acceleration technique such as the multigrid method. A coarse-grid generation method using octree data of the Cartesian grid is proposed. This method is simple and it can generate high-quality coarse grids. The other is a programing technique such as data structure improvement and performance tuning. We demonstrate the high-speed performance of the code for aerodynamic computation of a standard aircraft model, NASA-CRM. The computational time is less than one hour using 10 million cells and 100 CPU cores. It is found that the multigrid method is beneficial for large-scale problems., 形態: 図版あり, Physical characteristics: Original contains illustrations, 資料番号: PA1520034000},
 pages = {96(20)--105(29)},
 title = {高速な非構造格子流体ソルバFaSTARの開発},
 volume = {63},
 year = {2015}
}