@inproceedings{oai:jaxa.repo.nii.ac.jp:00005441,
 author = {郭, 東潤 and 中畠, 浩二 and 石川, 敬掲 and 野口, 正芳 and 吉田, 憲司 and Kwak, Dong-Youn and Nakahata, Koji and Ishikawa, Hirotaka and Noguchi, Masayoshi and Yoshida, Kenji},
 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), A supersonic flight test was conducted by JAXA to validate the aerodynamic design technology of the supersonic transport. Surface static pressure distributions and aerodynamic forces of the supersonic experimental airplane (NEXST-1) were obtained by the flight test. Flight test data were analyzed with high accuracy, and were evaluated by comparing with the CFD analysis. Relatively good agreements were observed with the flight test results and the CFD results. The validity of the drag reduction design concepts and design tools were confirmed from the flight test., 形態: カラー図版あり, 資料番号: AA0064239005, 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 = {飛行実験における力及び圧力特性解析},
 volume = {JAXA-SP-08-008},
 year = {2009}
}