並列タイトル等Calculation of High Speed Flow about Winged 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-9
一般注記The objective of the present study is to numerically calculate the flow about the fundamental configuration for flying vehicle at high speed: supersonic and hypersonic regimes. Two kinds of body configurations were chosen: a hemisphere-cylinder and a shuttle-like body. In the present study three numerical schemes are employed to compare each result: the Beam-Warming method, the Yee-Harten TVD method and the MacCormack TVD method. Furthermore, those results are compared with experiment which was conducted by the shock tunnel at Nagoya University at M=8 The reasonable agreement was obtained between them for the location of bow shock wave, which validates the present simulation.
資料番号: NALSP0009022
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=43313&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