@inproceedings{oai:jaxa.repo.nii.ac.jp:00005444,
 author = {郭, 東潤 and 黒田, 文武 and 伊藤, 健 and 徳川, 直子 and 石川, 敬掲 and 中畠, 浩二 and 野口, 正芳 and 上田, 良稲 and 吉田, 憲司 and Kwak, Dong-Youn and Kuroda, Fumitake and Ito, Takeshi and Tokugawa, Naoko and Ishikawa, Hirotaka and Nakahata, Koji and Noguchi, Masayoshi and Ueda, Yoshine 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), An aerodynamic database system named the NEXST-DB was constructed by JAXA to contribute on the aerospace research area in Japan. A number of aerodynamic data on the supersonic experimental airplane (NEXST-1) can be accumulated by the NEXST project. Three kinds of data of the pressure distribution, aerodynamic forces and boundary layer transitions were carried on the NEXST-DB. These aerodynamic data were obtained from the flight test, CFD analysis and wind tunnel tests. Furthermore, the geometry data of the NEXST-1 and the grid data for CFD analysis were also carried on the NEXST-DB. Those data can download on the website., 形態: カラー図版あり, 資料番号: AA0064239008, 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 = {ロケット実験機の空力データベース概要},
 volume = {JAXA-SP-08-008},
 year = {2009}
}