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고체 연료 추진제 내부 물리 현상에 대한 유체-구조-연소 통합 해석 : Full burning ALE based Fluid-Structure-combustion Interaction simulation for solid propellant rocket interior
DC Field | Value | Language |
---|---|---|
dc.contributor.author | 한상호 | - |
dc.contributor.author | 이창수 | - |
dc.contributor.author | 김종암 | - |
dc.creator | 김종암 | - |
dc.date.accessioned | 2013-08-02T05:16:25Z | - |
dc.date.available | 2013-08-02T05:16:25Z | - |
dc.date.issued | 2013-02-28 | - |
dc.identifier.citation | 제12회 우주발사체기술 심포지움, pp. 1-6 | - |
dc.identifier.uri | https://hdl.handle.net/10371/83227 | - |
dc.description.abstract | A fluid-structure interaction simulation of solid propellant rocket interior is carried out by employing the ALE (Arbitrary Lagrangian Eulerian) description, a hybrid model of continuum motion description combining the advantages of classical Lagrangian and Eulerian description. The integration process for fluid-structure interaction and an automatic re-meshing algorithm are included to analyze an unsteady fluid-structure interaction phenomenon with the deformation of solid grain during the simulation. The developed solver is applied for the full burning simulation of a solid propellant grain, which is a highly-coupled unsteady phenomenon between gas flow and propellant structure. Based on the integrated computed results, flow physics in the combustion chamber and the behavior of a solid propellant deformation are examined. | - |
dc.language.iso | ko | en |
dc.publisher | 한국항공우주학회 | en |
dc.subject | 공학 | en |
dc.subject | Solid Propellant Rocket | - |
dc.subject | 고체 추진 로켓 | - |
dc.subject | Fluid Structure Interaction | - |
dc.subject | 유동 구조 연동 해석 | - |
dc.subject | Arbitrary Lagrangian Eulerian | - |
dc.subject | ALE 기법 | - |
dc.title | 고체 연료 추진제 내부 물리 현상에 대한 유체-구조-연소 통합 해석 | en |
dc.title.alternative | Full burning ALE based Fluid-Structure-combustion
Interaction simulation for solid propellant rocket interior | - |
dc.type | Conference Paper | - |
dc.author.alternative | Han, Sangho | - |
dc.author.alternative | Lee, Changsoo | - |
dc.author.alternative | Kim, Chongam | - |
dc.description.srnd | OAIID:oai:osos.snu.ac.kr:snu2013-01/104/0000004648/3 | - |
dc.description.srnd | SEQ:3 | - |
dc.description.srnd | PERF_CD:SNU2013-01 | - |
dc.description.srnd | EVAL_ITEM_CD:104 | - |
dc.description.srnd | USER_ID:0000004648 | - |
dc.description.srnd | ADJUST_YN:N | - |
dc.description.srnd | EMP_ID:A001138 | - |
dc.description.srnd | DEPT_CD:446 | - |
dc.description.srnd | CITE_RATE:0 | - |
dc.description.srnd | FILENAME:2013우주발사체기술심포지움_한상호.pdf | - |
dc.description.srnd | DEPT_NM:기계항공공학부 | - |
dc.description.srnd | EMAIL:chongam@snu.ac.kr | - |
dc.description.srnd | CONFIRM:Y | - |
dc.identifier.srnd | 2013-01/104/0000004648/3 | - |
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