@inproceedings{oai:jaxa.repo.nii.ac.jp:00004723,
 author = {坂下, 雅秀 and 松尾, 裕一 and 橋本, 敦 and 青山, 剛史 and Sakashita, Masahide and Matsuo, Yuichi and Hashimoto, Atsushi and Aoyama, Takashi},
 book = {宇宙航空研究開発機構特別資料: 第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 論文集, JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010},
 month = {Feb},
 note = {第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP), 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25,  2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan, We apply the GMRES method with LU-SGS right preconditioning, faster and more stable than the LU-SGS method, to the three dimensional hybrid-unstructured grid finite-volume method flow solver FaSTAR(FaST Aerodynamic Routines), and compare the execution time with LU-SGS method by ONERA M6 wing simulation. As a result, we confirm the GMRES method is about 2 times faster than LU-SGS method., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064967016, レポート番号: JAXA-SP-10-012},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {LU-SGS右前処理付きGMRES法の高速流体ソルバFaSTARへの適用},
 volume = {JAXA-SP-10-012},
 year = {2011}
}