@inproceedings{oai:jaxa.repo.nii.ac.jp:00003832,
 author = {古賀, 星吾 and 廣谷, 智成 and 田口, 秀之 and 藤川, 貴弘 and 要田, 大輔 and 早坂, 陽 and 土屋, 武司 and Koga, Seigo and Hirotani, Tomonari and Taguchi, Hideyuki and Fujikawa, Takahiro and Kanameda, Daisuke and Hayasaka, Akira and Tsuchiya, Takeshi},
 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), Wind tunnel tests to obtain low-speed aerodynamic characteristics of a hypersonic passenger aircraft were conducted at the JAXA 2m×2m Low-Speed Wind Tunnel. The wind tunnel test model has an electric ducted fun (EDF) engine. This paper mainly describes improved methods for wind tunnel tests with an EDF engine and examples of the application., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530024013, レポート番号: JAXA-SP-14-011},
 pages = {68--71},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {HST低速性能実験機の電動ファンエンジン駆動を伴う風洞試験について: その2},
 volume = {JAXA-SP-14-011},
 year = {2015}
}