並列タイトル等Numerical Analysis of Inviscid Flows about Wing-Fuselage Combinations II. Development of Full Potential Flow Code YOKUDO-P
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-881
一般注記The main purpose of this paper is to numerically analyse inviscid flows about wing-fuselage combinations. In the second series we present a numerical procedure for calculating full potential flows about wing-fuselage combinations by the successive-line-over-relaxation method of the rotated finite difference scheme, using the grids which have already been generated by the code YOKUDO-G in the first series. A user’s manual for the FORTRAN code of the procedure is also described. Furthermore, many numerical examples are presented in order to show the utility of this code for flows about several wing-fuselage combinations under several free stream boundary conditions. The numerical results obtained by this code are compared with the experimental results and with numerical results of other methods.
資料番号: NALTR0881000
レポート番号: NAL TR-881
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45139&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