並列タイトル等Application of Computational Aerodynamics to Wing Design
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-3
一般注記Recent progress in Computational Aerodynamics has enabled the engineers of air-craft manufacturers to utilize transonic aerodynamic analysis programs in designing wings. When using these programs in wing design, points like (Configuration modelling) effects of fuselage, effects of control surfaces, effects of nacelle, etc (Computational method) effects of viscosity, effects of separation, etc. should be taken into account to select a program or to model a configuration. Effectiveness of control surfaces (spoiler, aileron), which is greatly influenced by the characteristics of the wing, is another important problem. This paper introduces application of transonic aerodynamic analysis programs to the computation of control surface effective-ness.
資料番号: NALSP0003032
レポート番号: NAL SP-3
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43174&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