| Title | Tensile test and simulation of woven composite laminates after high velocity impact |
| Creator | |
| Date Issued | 2014 |
| Source Publication | Advanced Materials Research
 |
| ISSN | 1022-6680 |
| Volume | 971-973 |
| Pages | 232-235 |
| Abstract | Tensile mechanical behaviors of two kinds composite laminates G803/5224 and G827/5224 specimen after high-speed impact were investigated separately. The influences of open-hole on the specimen's net tensile strength were analyzed by comparing with standard specimen's experimental results. An FEM model was established to simulate the damage growth in the laminates. Different equivalent zones were applied to model different velocity impact damages, and different damage criteria and modulus attenuation rules were used for two different ply forms. © (2014) Trans Tech Publications, Switzerland. |
| Keyword | Composite laminates Impact failure Simulation analysis Tensile test |
| DOI | 10.4028/www.scientific.net/AMR.971-973.232 |
| URL | View source |
| Language | 英语English |
| Scopus ID | 2-s2.0-84904194806 |
| Citation statistics | |
| Document Type | Conference paper |
| Identifier | http://repository.uic.edu.cn/handle/39GCC9TT/12314 |
| Collection | Research outside affiliated institution |
| Affiliation | School of Aeronautic Science and Engineering, BEIHANG UNIV.,Beijing, 100191,China |
| Recommended Citation GB/T 7714 | Ge，Ming Ming,Cheng，Xiao Quan,Zhang，Qianet al. Tensile test and simulation of woven composite laminates after high velocity impact[C], 2014: 232-235. |
| Files in This Item: | There are no files associated with this item. | |||||
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