並列タイトル等Numerical Simulation of Wing in Grand Effect II
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Flow around a wing in ground effect is studied by solving both the incompressible and compressible Navier-Stokes equations numerically. Standard MAC method with third order upwind difference for non-linear term is used to calculate incompressible flow. For compressible flow, a new numerical scheme is developed. Both scheme run well and we can investigate numerically the effect of the distance from the ground, that of attack angle and that of the oscillation of the wing, on the flow field and the force acting on the body.
資料番号: NALSP0010041
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=43370&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