1. Aerodynamic database of the supersonic experimental airplane (NEXST-1) in JAXA
- Author
-
Kwak, Dong-Youn, Kuroda, Fumitake, Ito, Takeshi, Tokugawa, Naoko, Ishikawa, Hirotaka, Nakahata, Koji, Noguchi, Masayoshi, Ueda, Yoshine, and Yoshida, Kenji
- Subjects
Database, Aerodynamics, Supersonic Transport - Abstract
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
- Published
- 2009