| contributor author | Justin D. Littell | |
| contributor author | Wieslaw K. Binienda | |
| contributor author | Gary D. Roberts | |
| contributor author | Robert K. Goldberg | |
| date accessioned | 2017-05-08T21:16:27Z | |
| date available | 2017-05-08T21:16:27Z | |
| date copyright | July 2009 | |
| date issued | 2009 | |
| identifier other | %28asce%290893-1321%282009%2922%3A3%28270%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45168 | |
| description abstract | Carbon fiber composites that utilize flattened, large tow yarns in woven or braided forms are being used in many aerospace applications. The complex fiber architecture and large unit cell size in these materials present challenges for both understanding the deformation process and measuring reliable material properties. In this paper composites made using flattened 12k and 24k (referring to the number of fibers in the fiber tow) standard modulus carbon fiber yarns in a | |
| publisher | American Society of Civil Engineers | |
| title | Characterization of Damage in Triaxial Braided Composites under Tensile Loading | |
| type | Journal Paper | |
| journal volume | 22 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2009)22:3(270) | |
| tree | Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 003 | |
| contenttype | Fulltext | |