@inproceedings{oai:jaxa.repo.nii.ac.jp:00038080,
 author = {真鍋, 圭司 and 瀬崎, 新士 and 西尾, 正富 and Manabe, Keiji and Sezaki, Shinji and Nishio, Masatomi},
 book = {航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001},
 month = {Jan},
 note = {The numerical simulation around a space plane traveling at the speed of Mach 10 was carried out based on FEM (Finite Element Method). In this FEM formulation, stress (pressure) term is partially integrated in an element by applying the weighted residual method, and the hypersonic flowfield around a space plane model including shock wave can be calculated. three-dimensional simulations were conducted for the case of the angle of attack is 0 and 10 deg. The simulation results are compared with experimental results obtained by the electric discharge method, and good correlation between them was found., 資料番号: AA0032819044, レポート番号: NAL SP-53},
 pages = {257--261},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {マッハ10で飛行するスペースプレーン周りの数値シミュレーション},
 volume = {53},
 year = {2002}
}