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Bibliographic Record
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- Material Type
- 規格・テクニカルリポート類
- Author/Editor
- 橋本, 雅方廣瀬, 直喜大貫, 武Hashimoto, MasakataHirose, NaokiOonuki, Takeshi
- Publication, Distribution, etc.
- Publication Date
- 1989-11
- Publication Date (W3CDTF)
- 1989-11
- Alternative Title
- Transonic Aerodynamics Analyses of Unconventional Wing Configurations by 3D-Euler Code
- Periodical title
- 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10
- No. or year of volume/issue
- 10
- Volume
- 10
- Pages
- 265-272
- ISSN (Periodical Title)
- ISSN : 0289-260X
- Text Language Code
- jpn
- Target Audience
- 一般
- Note (General)
- 出版タイプ： NANew 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
- Periodical Title (NCID)
- AN10097345
- Data Provider (Database)
- 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）
- Original Data Provider (Database)
- 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