JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
62304000.pdf6.42 MB
titleTransonic Wind Tunnel Test of the NASA CRM: Volume 1
Author(jpn)上野, 真; 香西, 政孝; 古賀, 星吾
Author(eng)Ueno, Makoto; Kohzai, Masataka; Koga, Seigo
Author Affiliation(jpn)宇宙航空研究開発機構航空本部(JAXA); 宇宙航空研究開発機構航空本部(JAXA); 宇宙航空研究開発機構航空本部(JAXA)
Author Affiliation(eng)Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA); Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA); Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)
Issue Date2014-03-31
Publisher宇宙航空研究開発機構(JAXA)
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
VolumeJAXA-RM-13-017E
Start page1
End page90
Publication date2014-03-31
Languageeng
AbstractA wind tunnel test of a 80% scale copy of the NASA Common Research Model (CRM) was performed in the 2m×2m transonic wind tunnel of the Japan Aerospace Exploration Agency (JAXA). JAXA consulted with NASA Langley Research Center and committee members of the Drag Prediction Workshop during the wind tunnel model fabrication. The test was conducted at the relatively low Reynolds number of 2.27×10(exp 6) due to limitations in the tunnel's capability, and boundary layer transition was simulated with optimized trip dots. Static pressure distributions and aerodynamic forces were successfully acquired from the test campaign, and the data were compared with those from the NASA National Transonic Facility. Numerical data acquired by JAXA are presented in this paper. This volume includes the results from wind tunnel tests conducted in 2012.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Document TypeTechnical Report
JAXA Category研究開発資料
NASA Subject CategoryAerodynamics
ISSN1349-1121
NCIDAA11983593
SHI-NOAA0062304000
Report NoJAXA-RM-13-017E
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/16455


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