@article{oai:jaxa.repo.nii.ac.jp:00022622,
 author = {村山, 光宏 and 横川, 譲 and 山本, 一臣 and 浦, 弘樹 and 今村, 太郎 and 平井, 亨 and 伊藤, 靖 and 郭, 東潤 and 小林, 宙 and 進藤, 重美 and Murayama, Mitsuhiro and Yokokawa, Yuzuru and Yamamoto, Kazuomi and Ura, Hiroki and Imamura, Taro and Hirai, Tohru and Ito, Yasushi and Kwak, Dongyoun and Kobayashi, Hiroshi and Shindo, Shigemi},
 issue = {APISAT-2013},
 journal = {Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan},
 month = {Nov},
 note = {This paper presents computational and experimental results on investigation of noise generation from the flap side-edge for high-lift device noise research models in JAXA. The main purpose of this paper is focused on investigation of the differences of the flow field between the models with and without the swept angle and taper-ratio of the wing by comparison of the computational results. In the case of wings with the swept angle and taper-ratio, the flap is deployed in a three-dimensional direction based on the wing planform. The changes of the behaviors of the vortices from the flap side-edge and resulting pressure fluctuations due to the flap deployment are shown., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: PA1520037000},
 pages = {a9--a16},
 title = {Investigation of Noise Generation from Bluff Flap Side-edge of a High-Lift Wing Model},
 volume = {12},
 year = {2014}
}