@inproceedings{oai:jaxa.repo.nii.ac.jp:00004394,
 author = {西村, 康孝 and 佐々木, 大輔 and 中橋, 和博 and Nishimura, Yasutaka and Sasaki, Daisuke and Nakahashi, Kazuhiro},
 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, Building Cube Method (BCM) is based on the Cartesian mesh. Cartesian mesh solver has critical problem to treat wall boundary, accurately. The immersed boundary method (IBM) has been studied to treat wall boundary. The immersed boundary method is a method to give the appropriate wall boundary condition to the object surface in order to solve the flow smoothly at near the body. Thus, the objective of this study is to establish a practical, efficient IBM-based Cartesian mesh solver, which achieves low computational costs and high accuracy to solve the flow around the wing. An immersed boundary method (IBM) using ghost cell and image point is implemented into the Cartesian mesh solver flow the compressible Euler equations to treat slip wall boundary condition. It is validated by computing inviscid flows around NACA0012 airfoil, RAE2822 airfoil and ONERA M6 wing., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207022, レポート番号: JAXA-SP-11-015},
 pages = {131--136},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {圧縮性Building Cube Methodを用いた翼周りのEuler解析},
 volume = {JAXA-SP-11-015},
 year = {2012}
}