| contributor author | Peter A. Gustafson | |
| contributor author | Anthony M. Waas | |
| date accessioned | 2017-05-08T21:33:47Z | |
| date available | 2017-05-08T21:33:47Z | |
| date copyright | July 2011 | |
| date issued | 2011 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000083.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56226 | |
| description abstract | This paper reports an experimental program to establish a cohesive zone model for the T650/AFR-PE-4 (laminate) and FM680-1 (adhesive) system. The cohesive zone model is based on a four parameter characterization: in each mode, a range of values for the critical energy release rate and cohesive strength are computed from a set of experimental results. Values of each parameter are determined over the temperature range of 20–350°C. Owing to experimental limitations, two methods for determining the Mode I critical energy release rate are reported from the double cantilever beam test: the area method and the inverse method. The Mode I strength is determined from a button peel stress test. The values of the Mode II parameters are determined by using a mapping procedure that accounts for multiparameter dependence in models of the end notch flexure and single lap joint tests. | |
| publisher | American Society of Civil Engineers | |
| title | Experiments and Cohesive Zone Model Parameters for T650/AFR-PE-4/FM680-1 at High Temperatures | |
| type | Journal Paper | |
| journal volume | 24 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000083 | |
| tree | Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003 | |
| contenttype | Fulltext | |