@inproceedings{oai:jaxa.repo.nii.ac.jp:00002940,
 author = {村山, 光宏 and 雨宮, 和久 and 田中, 健太郎 and 伊藤, 靖 and 横川, 譲 and 山本, 一臣 and 池田, 友明 and 平井, 亨 and Murayama, Mitsuhiro and Amemiya, Kazuhisa and Tanaka, Kentaro and Ito, Yasushi and Yokokawa, Yuzuru and Yamamoto, Kazuomi and Ikeda, Tomoaki and Hirai, Toru},
 book = {宇宙航空研究開発機構特別資料: 第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium},
 month = {Feb},
 note = {第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎, 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan, Aeroacoustic simulations associated with noise radiation from the leading-edge slat is conducted. The shear layer emanating from the slat cusp and its subsequent reattachment upstream of the slat trailing edge lead to a primarily broadband noise spectrum. Often, however, the slat noise spectrum also exhibits narrowband peaks superimposed on the broadband portion, especially in the case of unswept wind tunnel configurations at lower than full-scale Reynolds numbers. In this study, influence of wing sweep angle on the slat noise characteristics, especially on the narrowband peaks, is investigated by aeroacoustic simulation using Delayed Detached Eddy Simulation around the 30P30N three-element high-lift airfoil configuration., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1830029011, レポート番号: JAXA-SP-18-005},
 pages = {121--126},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {翼後退角有無によるスラット騒音変化について},
 volume = {JAXA-SP-18-005},
 year = {2019}
}