@inproceedings{oai:jaxa.repo.nii.ac.jp:00006555,
 author = {横川, 譲 and 青木, 良尚 and 森田, 義郎 and 高橋, ひとし and 星野, 秀雄 and 室田, 勝一 and 野中, 修 and 真城, 仁 and 遠藤, 亮 and 吉田, 憲司 and Yokokawa, Yuzuru and Aoki, Yoshinao and Morita, Yoshio and Takahashi, Hitoshi and Hoshino, Hideo and Murota, Katsuichi and Nonaka, Osamu and Mashiro, Jin and Endo, Atsushi and Yoshida, Kenji},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第33回・第34回, JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition},
 month = {Jan},
 note = {The work described here relates to the method measuring the boundary layer transition at large-scale and low-speed wind tunnel. The objective of the research is to improve the test technique and to know a precise procedure about transition measurements, especially for an aircraft model at such type of wind tunnel. At JAXA 6.5 m x 5.5 m Low-Speed Wind Tunnel (LWT1), the boundary layer growing on the left-wing of the ONERA-Model was investigated using two kinds of the quantitative methods (Preston Tube and Hotfilm Sensor) and also two kinds of the visualizing methods (Temperature-Sensitive Liquid Crystal, Infrared Camera). Throughout the experiment, a lot of knowledge were obtained. Transition points investigated by four kinds of methods were correctively agreed., 資料番号: AA0047776001, レポート番号: JAXA-SP-04-002},
 pages = {1--4},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {6.5mx5.5m低速風洞における全機模型遷移計測の試み},
 volume = {JAXA-SP-04-002},
 year = {2005}
}