並列タイトル等Finite Difference Numerical Prediction of Aerodynamics for Airfoil Flying Over Wavy Wall
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-14
一般注記The lift on an airfoil flying over a wavy wall surface is calculated using a finite difference method, which was developed by J. Nakamichi1) to improve LTRAN2 evolved by W.F. Ballhaus & P.M. Goorjian2). Numerical computations include cases of a flat plate over a flat solid wall prior to the cases of a moving wavy wall. Modification of grid generating system is the major point for applying Nakamichi's method to our problem. The weak compressibility (M infinity =0.1-0.3) is considered but non-linearity is neglected in our calculations. The calculated results are compared with those obtained by the lifting surface theory of M. Ichikawa et al.3) The agreements are quite satisfactory.
資料番号: NALSP0014013
レポート番号: NAL SP-14
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43446&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