@techreport{oai:jaxa.repo.nii.ac.jp:00002502,
 author = {上野, 真 and 香西, 政孝 and 古賀, 星吾 and Ueno, Makoto and Kohzai, Masataka and Koga, Seigo},
 month = {Mar},
 note = {A 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062304000, レポート番号: JAXA-RM-13-017E},
 title = {Transonic Wind Tunnel Test of the NASA CRM: Volume 1},
 year = {2014}
}