Two-Dimensional Analysis of Coanda Effect in Ideal Fluid

• 資料種別: 規格・テクニカルリポート類
• タイトル: Two-Dimensional Analysis of Coanda Effect in Ideal Fluid
• 著者・編者: 高沢, 金吾; TAKASAWA, Kingo
• 著者標目: 高沢, 金吾; TAKASAWA, Kingo
• 出版事項: 航空宇宙技術研究所
• 出版年月日等: 1986-04
• 出版年（W3CDTF）: 1986-04
• 並列タイトル等: 理想流体を想定したコアンダ効果の2次元解析
• タイトル（掲載誌）: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-904
• 巻号年月日等（掲載誌）: 904
• 掲載巻: 904
• 掲載ページ: 12-
• ISSN（掲載誌）: ISSN : 0389-4010
• 本文の言語コード: eng
• 対象利用者: 一般
• 一般注記: 出版タイプ： NA; The Coanda effect, or the phenomenon of a jet running along a curved wall is analysed with a two-dimensional approach assuming an ideal fluid. A thick jet emerging from a nozzle with an arbitrary kick down angle is mainly concerned, relative to the upper-surface-blowing high lift concept. The result of the free stream line analysis of a jet running along an infinite plane wall is conformally transformed under the constraint of the conservation of the free stream line condition, and the Coanda flow along the curved wall is deduced. Not only the shaped of the stream lines but also the flow velocity vector diagram and the wall pressure coefficient are calculated. The effect of the finiteness of a plane wall or the existence of the trailing edge of a wing/flap is also evaluated. Computation is executable with a 16-bit desk top computer, and programs written in the BASIC language are available.; 資料番号: NALTR0904000; レポート番号: NAL TR-904
• 連携機関・データベース: 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）; https://irdb.nii.ac.jp
• 提供元機関・データベース: 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ