並列タイトル等Numerical Simulation of Flow Fields around a Airplane of Complex Geometries
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A numerical aerodynamic simulation system applicable to various complex geometries was developed. We use an O-O type of grid in order to concentrate grid points in wall boundary layers effectively and to implement wall and outer boundary conditions easily. In addition, on the body surface, the grid is devided into several blocks which have common points at each interface. By doing so, a finite volume algorithm can be applied easily and the Navier-Stokes code using this grid became adaptable to various kinds of airplanes. As a first example, we tried to compute the flowfield around a practical aircraft configuration, and also compared the solution with the wind tunnel test data.
資料番号: NALSP0010033
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=43362&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