@inproceedings{oai:jaxa.repo.nii.ac.jp:00006644,
 author = {高木, 亮治 and 鈴木, 教雄 and Takaki, Ryoji and Suzuki, Norio},
 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 = {This paper presents continuous efforts of EFC/CFD validation for supersonic flows around NEXST-1. Among them, two topics will be mainly described here. One is an analysis on the measured geometry of the wind tunnel model, showing that discrepancies of pressure distributions are due to the discrepancy of the model geometry. This is remarkable at the outer region of the wing. The other is a simulation with transition. The transition model which was used in previous works cannot occur the transition exactly where it is wanted. Another model used in this work can improve the problem. The analysis with the transition model decreases the discrepancy between CFD results and EFD data., 資料番号: AA0047427043, レポート番号: JAXA-SP-03-002},
 pages = {244--249},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {NEXST-1周りの超音速流解析結果の検証:第3回SST-WSでのコンペティションの結果の詳細検討},
 volume = {JAXA-SP-03-002},
 year = {2004}
}