A Study on Separating Force between Laminate Composite Part and Tool

摘要：

The precise dimension ofa finished composite strongly depends on the part and tool interactions. The interactions mostly arise due to difference between coefficients of thermal expansion (CTEs) of the part and tool. In this study, the thermal interaction between composite part and composite tool is investigated experimentally and computationally.

关键词： separating force double cantilever beam (DCB) finite element method energy release rates laminate composite

作者: Lee Sangkyo Lee Mingyu Cho Chongdu Ansari M Z. Kim Seung chul Kim Dae sung

作者单位: Department of Mechanical Engineering, Inha University, Incheon, Korea Korea Institute of Aeronautical Technology,Korean-air,Deajeon, Korea Commercial Aerospace Plant Aerospace Division, Korean-air,Busan,Korea

会议类型: 国际会议

会议名称: 2010 Asia-Pacific International Symposium on Aerospace Technology(2010 亚太航空航天技术研讨会 APISAT 2010)

会议地点: 西安

会议语种:英文

页码: 836-839

在线出版日期: 2010-09-01（万方平台首次上网日期，不代表论文的发表时间）