並列タイトル等Supersonic Flow on Axisymmetric Blunt Body
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-3
一般注記Inviscid supersonic flows around axisymmetric indented bodies are numerically analyzed by the Implicit MacCormack scheme. The scheme has been developed for the strong conservative form of Euler equation. Grid generation by elliptic P. D. E. has been employed for relatively complicated body-shapes. The free stream Mach number ranged from 1.8 to 8.0. Various body shapes are treated in this paper such as a sphere, an indented body, and a hemisphere cylinder. Some details of the formation of the scheme are described and it is observed that the method is highly efficient except for the region near the stagnation point.
資料番号: NALSP0003001
レポート番号: NAL SP-3
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43143&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