| contributor author | Bin Yang | |
| contributor author | Kunkun Fu | |
| contributor author | Yan Li | |
| date accessioned | 2022-05-07T21:26:49Z | |
| date available | 2022-05-07T21:26:49Z | |
| date issued | 2022-03-09 | |
| identifier other | (ASCE)AS.1943-5525.0001417.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4283735 | |
| description abstract | This study presents a finite-element (FE) model considering intralaminar damage and interlaminar delamination to predict the biaxial compression behavior of carbon fiber–reinforced composites (CFRCs) with low-velocity impact damage. First, the FE model was validated by a uniaxial compression experiment. The FE predictions in terms of compression after impact (CAI) strength and failure patterns were consistent with the experimental results. Then the validated FE model was used to predict the biaxial compression behavior of the CFRCs. It was found that the residual strength of the CFRCs was dependent on the buckling mode of the laminate due to the coupling effect of the longitudinal and transverse compressive loadings. Correspondingly, the CAI strength under biaxial compression was lower than that under longitudinal or transverse compressive loading. | |
| publisher | ASCE | |
| title | Modeling of Biaxial Compression Behavior of Carbon Fiber–Reinforced Composite after Low-Velocity Impact | |
| type | Journal Paper | |
| journal volume | 35 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0001417 | |
| journal fristpage | 04022024 | |
| journal lastpage | 04022024-12 | |
| page | 12 | |
| tree | Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 003 | |
| contenttype | Fulltext | |
