並列タイトル等Numerical Simulation of Flow Around the Aircraft Designed to Utilize Ground Effect
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-9
一般注記Flow around an aircraft spatially designed to taking advantage of ground effect effectively is studied by using the incompressible Navier-Stokes equations. Third-order upwind difference scheme is used to solve the equations. Calculations are carried out under many conditions, i.e. the distance from the body to the ground, the angle of attack and the Reynolds number, etc. are changed systematically in order to investigate these effects on the flow field and force acting on the body.
資料番号: NALSP0009033
レポート番号: NAL SP-9
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43324&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