小型二段式ロケットの前後翼間の空力干渉による垂直力について

• 資料種別: 文書・図像類
• タイトル: 小型二段式ロケットの前後翼間の空力干渉による垂直力について
• 著者・編者: 白水, 正男; 曽我, 国男; 柴藤, 羊二; 秋元, 敏男; SHIROUZU, Masao; SOGA, Kunio; SHIBATO, Yoji; AKIMOTO, Toshio
• 著者標目: 白水, 正男; 曽我, 国男; 柴藤, 羊二; 秋元, 敏男; SHIROUZU, Masao; SOGA, Kunio; SHIBATO, Yoji; AKIMOTO, Toshio
• 出版事項: 航空宇宙技術研究所
• 出版年月日等: 1984-05
• 出版年（W3CDTF）: 1984-05
• 並列タイトル等: An Experimental Study on the Induced Normal Force on Tail-Fins due to Wing-Tail Interference
• 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-814
• 巻号年月日等（掲載誌）: 814
• 掲載巻: 814
• 掲載ページ: 18-
• 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: The normal force on the tail-fins induced by aerodynamic load on front-fins was studied. The magnitude of the induced normal force was obtained experimentally from a wind tunnel test of two-stage rocket models with both front- and tail-fin, with either front- or tail-fin, and without any fin. The test was performed at M∞ = 0.5 ～ 0.95 and 1.5～2.5, and the induced normal force in this region was about 30％, at maximum, of the normal force which acts on the entire model. The variation of the induced normal force with bank angle difference between front- and tail-fin was also obtained from wind tunnel tests of a roll-controllable rocket model at M∞ = 0.50 ～ 1.20. Those results were compared with predictions based on the strip theory. This simplified theory succeeded in giving approximate magnitude and Mach number dependence of the induced normal force ; however, it is not sufficient for precise prediction.; 資料番号: NALTR0814000; レポート番号: NAL TR-814
• 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