Combustion simulations at Computational Science Research Group

Autor:	Shinjo, Junji
Jazyk:	japonština
Rok vydání:	2006
Předmět:	火炎伝播 火炎構造 flame structure flow distribution 同軸ノズル 流れの分布 supercritical combustion 推薬燃焼 liquid atomization flame propagation 液体微粒化 liquid oxygen propellant combustion ロケットエンジン設計 liquid propellant rocket engine 液体酸素 rocket engine design coaxial nozzle 液体燃料ロケットエンジン 超臨界燃焼
Zdroj:	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. :87-88
ISSN:	1349-113X
Popis:	This 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
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::591f5d2bbb3cf4f9fca7f9fb6a65f73b http://id.nii.ac.jp/1696/00005996/ Zobrazit plný text záznamu