| contributor author | C. S. Chu | |
| date accessioned | 2017-05-08T21:15:38Z | |
| date available | 2017-05-08T21:15:38Z | |
| date copyright | January 1991 | |
| date issued | 1991 | |
| identifier other | %28asce%290893-1321%281991%294%3A1%2878%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44697 | |
| description abstract | Three materials, E‐glass, Kevlar, and S‐glass, are assessed in terms of their effectiveness as softening strips in the fail‐safe design of composite structures. The softening effect is assessed in terms of its influence on the failure behavior of AS/3501‐6 graphite‐epoxy laminates consisting of 16 plies in a lay‐up of | |
| publisher | American Society of Civil Engineers | |
| title | Crack Arrest and Residual Strength of Composite Panels with Softening Strips | |
| type | Journal Paper | |
| journal volume | 4 | |
| journal issue | 1 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(1991)4:1(78) | |
| tree | Journal of Aerospace Engineering:;1991:;Volume ( 004 ):;issue: 001 | |
| contenttype | Fulltext | |
