垂直孔多孔壁の二次元揚力干渉に関する実験

• 資料種別: 文書・図像類
• タイトル: 垂直孔多孔壁の二次元揚力干渉に関する実験
• 著者・編者: 沢田, 秀夫; 三堀, 進; 佐藤, 衛; 鈴木, 弘一; 細江, 信幸; SAWADA, Hideo; MITSUBORI, SUSUMU; SATO, Mamoru; SUZUKI, Koichi; HOSOE, Nobuyuki
• 著者標目: 沢田, 秀夫; 三堀, 進; 佐藤, 衛; 鈴木, 弘一; 細江, 信幸; SAWADA, Hideo; MITSUBORI, SUSUMU; SATO, Mamoru; SUZUKI, Koichi; HOSOE, Nobuyuki
• 出版事項: 航空宇宙技術研究所
• 出版年月日等: 1979-03
• 出版年（W3CDTF）: 1979-03
• 並列タイトル等: An Experiment of Lift Interference on 2-Dimensional Wings in a Wind Tunnel with Perforated Walls
• 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-563
• 巻号年月日等（掲載誌）: 563
• 掲載巻: 563
• 掲載ページ: 6-
• ISSN（掲載誌）: ISSN : 0389-4010
• 本文の言語コード: jpn
• 対象利用者: 一般
• 一般注記: An experiment on wall interference caused by the lift with two-dimensional wings, was carried out in the NAL 2m × 2m transonic wind tunnel with perforated walls, at high subsonic speeds. The open area ratios of upper and lower test section walls were set at 20％. Two airfoil models were used. In this experiment, pressure distributions near the upper and lower walls inside the test section were also measured, in addition to the pressure distribution on an airfoil model. Various quantities of lift interference with two-dimensional wings were assessed by a new method. This method was proposed in a previous paper, by one of the present authors, and requires only the measurement of pressure distributions on flow boundaries. Lift interference parameters, δ0 and δ1, for the present case, were evaluated indirectly by this method.; 資料番号: NALTR0563000; レポート番号: NAL TR-563
• 一次資料へのリンクURL: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44817&item_no=1&attribute_id=31&file_no=1
• オンライン閲覧公開範囲: 限定公開
• 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