JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
Other TitleAerodynamic Analysis Validation of TRANAIR++ applied to NEXST-1 configuration
Author(jpn)牧本, 卓也; 牧野, 好和
Author(eng)Makimoto, Takuya; Makino, Yoshikazu
Author Affiliation(jpn)菱友システムズエンジニアリングソリューション事業部; 宇宙航空研究開発機構航空プログラムグループ超音速機チーム (JAXA)
Author Affiliation(eng)Engineering Solutions Division, Ryoyu Systems; Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)
Issue Date2012-03-30
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発資料
JAXA research and development memorandum
Start page1
End page47
Publication date2012-03-30
AbstractJAXA supersonic transport team has introduced the commercially available full potential aerodynamic solver TRANAIR++ since 2008 for aerodynamic design and aerodynamic characteristics evaluation of a supersonic research airplane. In order to check the accuracy and efficiency of the TRANAIR++, it is applied to the scaled supersonic experimental airplane NEXST-1 which was designed, built, and used for flight test in 2005 to demonstrate JAXA's CFDbased inverse design technology and some supersonic low-drag design concepts. The aerodynamic characteristics from subsonic to supersonic speed regime of the NEXST-1 evaluated by the TRANAIR++ are compared to the CFD analysis results which are open to the public through the database named NEXST-DB.
DescriptionPhysical characteristics: Original contains color illustrations
形態: カラー図版あり
Keywordsaerodynamic analysis; full potential equation; supersonic transport
Document TypeTechnical Report
JAXA Category研究開発資料
Report NoJAXA-RM-11-015

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