@inproceedings{oai:jaxa.repo.nii.ac.jp:00006624,
 author = {今村, 太郎 and 鈴木, 宏二郎 and 中村, 孝 and 吉田, 正廣 and Imamura, Taro and Suzuki, Kojiro and Nakamura, Takashi and Yoshida, Masahiro},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {The Lattice Boltzmann Method (LBM) has been developed as new CFD tool, and is applied to various flow problems. In this paper, numerical simulation of flows around an airfoil is performed using Generalized Interpolation-based Lattice Boltzmann Method (GILBM), which is a LBM solver on generalized coordinates. Flows around three different airfoils, which were workshop problems of ANSS2000, are solved using the GILBM. Each airfoil has different stall patterns; trailing edge stall (NACA63(sub 3)-018), leading edge stall (NACA63(sub 1)-012), and thin airfoil stall (NACA64(sub A)-006). The present results show good agreement in Cl, Cd and Cp distribution with the experimental results at low angle of attack. By combining GILBM solver and Baldwin-Lomax turbulence model, the present results show the ability to predict the trailing edge stall., 資料番号: AA0047427023, レポート番号: JAXA-SP-03-002},
 pages = {125--130},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {一般座標系格子ボルツマン法による翼周り流れの数値計算},
 volume = {JAXA-SP-03-002},
 year = {2004}
}