@inproceedings{oai:jaxa.repo.nii.ac.jp:00005442,
 author = {石川, 敬掲 and 吉田, 憲司 and 郭, 東潤 and 川上, 浩樹 and 徳川, 直子 and Ishikawa, Hirotaka and Yoshida, Kenji and Kwak, Dong-Youn and Kawakami, Hiroki and Tokugawa, Naoko},
 book = {宇宙航空研究開発機構特別資料: 小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告, JAXA Special Publication},
 month = {Feb},
 note = {小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館), Flight test on supersonic experimental airplane (NEXST-1) was conducted successfully by Japan Exploration Agency on October, 2005. A lot of aerodynamic data on the flight test were obtained. In this study those flight test data were compared with the numerical analysis to validate the design technologies. The effect of the additional parts, the aeroelastic deformation and boundary layer transition were taken into account in the CFD analysis for higher accuracy. Then this comparison highlighted the quantitative benefit of the natural laminar flow wing design concept., 形態: カラー図版あり, 資料番号: AA0064239006, レポート番号: JAXA-SP-08-008},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {飛行実験におけるCFD解析},
 volume = {JAXA-SP-08-008},
 year = {2009}
}