並列タイトル等Transonic Aerodynamics Analyses of Unconventional Wing Configurations by 3D-Euler Code
タイトル(掲載誌)航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10
一般注記New wing configurations such as a forward-swept-wing and a joined-wing recently attract attentions and are studied with expectations for higher lift-to-drag ratio, wider range of aileron effectiveness or higher drag divergence Mach number than the conventional ones. In this report, a computational code especially developed for analyzing the transonic aerodynamics of the new wing configurations is presented. The code is based on a system of Euler equations which is solved by the time-split MacCormack's scheme. Computational results of lift, drag and pressure distributions characteristics of the forward-swept-wing and the joined-wing configurations are shown and discussed in comparison with those of the conventional aft-swept wing.
資料番号: NALSP0010044
レポート番号: NAL SP-10
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43373&item_no=1&attribute_id=31&file_no=1
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)
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