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Integrated FScI Computations of Internal Solid Rocket from Initial to Full Burning Phase
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Han, Sangho | - |
dc.contributor.author | Kim, Chongam | - |
dc.creator | 김종암 | - |
dc.date.accessioned | 2013-04-23T06:25:45Z | - |
dc.date.available | 2013-04-23T06:25:45Z | - |
dc.date.issued | 2012-10-11 | - |
dc.identifier.citation | The 9th Asian Computational Fluid Dynamics Conference, 2012. 10.10 - 10.14, Nanjing University of Aeronautics and Astronautics, China | - |
dc.identifier.uri | https://hdl.handle.net/10371/82332 | - |
dc.description.abstract | A fluid-structure interaction 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 fluid-structure interaction process 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 | - |
dc.language.iso | en | en |
dc.publisher | Asian Computational Fluid Dynamics | en |
dc.subject | 공학 | en |
dc.title | Integrated FScI Computations of Internal Solid Rocket from Initial to Full Burning Phase | en |
dc.type | Conference Paper | - |
dc.contributor.AlternativeAuthor | 한상호 | - |
dc.contributor.AlternativeAuthor | 김종암 | - |
dc.description.srnd | OAIID:oai:osos.snu.ac.kr:snu2012-01/104/0000004648/27 | - |
dc.description.srnd | SEQ:27 | - |
dc.description.srnd | PERF_CD:SNU2012-01 | - |
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:Integrated FScI Computations of Internal Solid Rocket from Initial to Full Burning Phase.pdf | - |
dc.description.srnd | DEPT_NM:기계항공공학부 | - |
dc.description.srnd | EMAIL:chongam@snu.ac.kr | - |
dc.description.srnd | CONFIRM:Y | - |
dc.identifier.srnd | 2012-01/104/0000004648/27 | - |
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