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Aerodynamic database of the supersonic experimental airplane (NEXST-1) in JAXA
- Source :
- 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.
- Publication Year :
- 2009
- Publisher :
- 宇宙航空研究開発機構, 2009.
-
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)<br />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.<br />形態: カラー図版あり<br />資料番号: AA0064239008<br />レポート番号: JAXA-SP-08-008
- Subjects :
- Database, Aerodynamics, Supersonic Transport
Subjects
Details
- Language :
- Japanese
- ISSN :
- 1349113X
- Database :
- OpenAIRE
- Journal :
- 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
- Accession number :
- edsair.jairo.........d5d8175e18ed000e64287b9ea50483eb