DC Field | Value | Language |
---|---|---|
dc.contributor.author | 주근수 | ko |
dc.contributor.author | 허훈 | ko |
dc.contributor.author | 정영혁 | ko |
dc.contributor.author | 윤종원 | ko |
dc.date.accessioned | 2018-12-20T05:58:28Z | - |
dc.date.available | 2018-12-20T05:58:28Z | - |
dc.date.created | 2018-12-13 | - |
dc.date.issued | 2018-06-15 | - |
dc.identifier.citation | 한국군사과학기술학회 2018 종합학술대회 | - |
dc.identifier.uri | http://hdl.handle.net/10203/248020 | - |
dc.description.abstract | This paper deals with a simulation technique to evaluate dynamic behavior of the projectile during a high impact test. The high impact test is utilized to verify safeties of inner components of projectiles at high speed of several hundred per second. The proposed simulation technique can consider thermal softening effect of a target material and automatic mesh generation method is applied to prevent mesh distortion of the target material. It is concluded that acceleration of the projectile has a good agreement between simulation and experimental results during the high impact test. | - |
dc.language | Korean | - |
dc.publisher | 한국군사과학기술학회, 국방과학연구소, 한양대학교 신호정보특화연구센터 | - |
dc.title | 열연화 현상 및 격자재구성법을 고려한 고충격시험의 해석기법 | - |
dc.title.alternative | Simulation Technique for a High Impact Test Considering Thermal Softening and Automatic Mesh Generation Method | - |
dc.type | Conference | - |
dc.type.rims | CONF | - |
dc.citation.publicationname | 한국군사과학기술학회 2018 종합학술대회 | - |
dc.identifier.conferencecountry | KO | - |
dc.identifier.conferencelocation | 제주 국제컨벤션센터 | - |
dc.contributor.localauthor | 허훈 | - |
dc.contributor.nonIdAuthor | 정영혁 | - |
dc.contributor.nonIdAuthor | 윤종원 | - |
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