@inproceedings{oai:jaxa.repo.nii.ac.jp:00036873,
 author = {大山, 健一 and Oyama, Kenichi},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Jan},
 note = {航空宇宙技術研究所 6-7 JUN. 1996 東京 日本, National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan, 触媒壁面上の非平衡流をシミュレートできる粘性衝撃層(VSL)法を開発した。OREX(軌道再突入実験機)周りの非平衡流シミュレーションの結果とOREX飛行データとの比較を通して、表面熱伝達への壁面触媒性の効果を推定した。, Viscous Shock Layer (VSL) method which is able to simulate nonequilibrium flows on catalytic walls was developed. In this study, the effect of the wall catalysis on the surface heat transfer was estimated through the comparison between the results of the nonequilibrium flow simulation around OREX (Orbital Reentry Experiment) and its flight data., 資料番号: AA0000685014, レポート番号: NAL SP-34},
 pages = {73--76},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {VSL法を用いたOREX周りの非平衡流解析},
 volume = {34},
 year = {1997}
}