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Bibliographic Record
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- Material Type
- 規格・テクニカルリポート類
- Title
- Author/Editor
- 新城, 淳史Shinjo, Junji
- Author Heading
- Publication, Distribution, etc.
- Publication Date
- 2006-11-01
- Publication Date (W3CDTF)
- 2006-11-01
- Alternative Title
- Combustion simulations at Computational Science Research Group
- Periodical title
- 宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
- No. or year of volume/issue
- JAXA-SP-06-006
- Volume
- JAXA-SP-06-006
- Pages
- 87-88
- ISSN (Periodical Title)
- ISSN : 1349-113X
- Text Language Code
- jpn
- Subject Heading
- Target Audience
- 一般
- Note (General)
- 出版タイプ： NAThis paper briefly summarizes numerical simulations related to rocket combustion at Computational Science Research Group, Institute of Aerospace Technology. The first part describes the investigation of a supercritical hydrogen flame of rocket injector element. The flame and flame-holding structures are elucidated by this simulation. The second part examines the droplet breakup mechanism due to capillary force. The influence of ligament end is included for new modeling. These results will lead to combustor system simulation in the future.資料番号: AA0049500018レポート番号: JAXA-SP-06-006
- Periodical Title (NCID)
- AA11984031
- Data Provider (Database)
- 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）
- Original Data Provider (Database)
- 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