@inproceedings{oai:jaxa.repo.nii.ac.jp:00003831,
 author = {青木, 良尚 and 西島, 寛典 and 安藤, 典久 and 平野, 貴司 and 渡辺, 光則 and 満尾, 和徳 and Aoki, Yoshihisa and Nishijima, Hironori and Ando, Norihisa and Hirano, Takashi and Watanabe, Mistunori and Mitsuo, Kazunori},
 book = {宇宙航空研究開発機構特別資料: 第86-第90回風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 86th-90th meeting},
 month = {Mar},
 note = {第90回風洞研究会議 (2014年5月22日-23日), Wind Tunnel Technology Association 90th Meeting (May 22-23, 2014), We conducted annual wind tunnel calibration test on November in 2013 in JAXA 1m by 1m supersonic wind tunnel. Mach number distribution at test section and aerodynamic longitudinal forces of AGARD-B standard model were measured in this test campaign. Mach number distribution and aerodynamic longitudinal forces with roughness generally used in development test matched the past data. And we found the tendency of forebody axial force coefficient without roughness changed., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530024012, レポート番号: JAXA-SP-14-011},
 pages = {64--67},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {JAXA 1m×1m 超音速風洞における2013年度気流検定試験結果},
 volume = {JAXA-SP-14-011},
 year = {2015}
}