@inproceedings{oai:jaxa.repo.nii.ac.jp:00004393,
 author = {菱田, 学 and 橋本, 敦 and 保江, かな子 and 村上, 桂一 and Hishida, Manabu and Hashimoto, Atsushi and Yasue, Kanako and Murakami, Keiichi},
 book = {宇宙航空研究開発機構特別資料: 第43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2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43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2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, Fast deformation method for unstructred grid is important in order to carry out Fluid-Structure Interaction simulation using several millions of cells in JAXA Digital/Analog Hybrid Wind Tunnel system. Algebraic schemes such as Surface Influence method have better prospects because of their high parallelization ability and easier implementation. In this paper, some algebraic schemes including Surface Influence method are investigated and proposed, and applied to DLR-F6 FX2B wind tunnel model simulation wilth static deformation., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207021, レポート番号: JAXA-SP-11-015},
 pages = {125--130},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {高速CFD空間格子変形法の検討},
 volume = {JAXA-SP-11-015},
 year = {2012}
}