並列タイトル等Numerical analysis of propellant feed systems in liquid-propellant rocket engines
タイトル(掲載誌)宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems
一般注記Numerical simulator for propellant feed systems in liquid-propellant rocket engines based on CFD is under development for supporting H-2A rocket and next generation rocket development. This simulator consists of turbo pump system simulator and tank system simulator. In this paper, the tank system simulator based on CIP-LSM, which computes free surface behavior, temperature and pressure in rocket propellant tank, is presented. Also, the computed results of 2D sloshing and broken dam problems are presented to assess the accuracy of the solver for problems with strong deformation of the fluid. The results were in good agreement with other published data and experiments. As a result, it was clear that CIP-LSM is an effective method for predicting strong deformation of free surface flows.
資料番号: AA0049056002
レポート番号: JAXA-SP-05-010
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6233&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