TY - JOUR
T1 - Failure prediction for fiber reinforced polymer composites based on virtual experimental tests
AU - Zhang, Binbin
AU - Ge, Jingran
AU - Cheng, Feng
AU - Huang, Jian
AU - Liu, Shuo
AU - Liang, Jun
N1 - Publisher Copyright:
© 2023 The Authors
PY - 2023/5/1
Y1 - 2023/5/1
N2 - A novel virtual experimental testing methodology that utilizes virtual microstructures representative of genuine fiber distribution, is devised to micromechanically simulate and scrutinize the inter-fiber failure of unidirectional (UD) carbon fiber reinforced polymer (CFRP) composites. The experimentally identified nonlinear behavior of the matrix is incorporated by utilizing the Drucker-Prager plasticity model. The interaction behavior between fiber-matrix interfaces, including delamination and friction, is represented by means of a cohesive interaction approach. The results of virtual testing demonstrate that interfacial parameters and the epoxy properties exert considerable influences on the predicted macroscopic responses under individual loading cases. Additionally, the interface and epoxy material properties are inversely determined through virtual testing analysis assisted by experimental results. Furthermore, the validated virtual testing method is utilized to obtain the inter-fiber failure envelope of the composites. The predictions are then compared with those theoretically derived from classical failure criteria. The current comparative studies indicate that the existing classical failure criterion exhibits limited predictive ability with computational data.
AB - A novel virtual experimental testing methodology that utilizes virtual microstructures representative of genuine fiber distribution, is devised to micromechanically simulate and scrutinize the inter-fiber failure of unidirectional (UD) carbon fiber reinforced polymer (CFRP) composites. The experimentally identified nonlinear behavior of the matrix is incorporated by utilizing the Drucker-Prager plasticity model. The interaction behavior between fiber-matrix interfaces, including delamination and friction, is represented by means of a cohesive interaction approach. The results of virtual testing demonstrate that interfacial parameters and the epoxy properties exert considerable influences on the predicted macroscopic responses under individual loading cases. Additionally, the interface and epoxy material properties are inversely determined through virtual testing analysis assisted by experimental results. Furthermore, the validated virtual testing method is utilized to obtain the inter-fiber failure envelope of the composites. The predictions are then compared with those theoretically derived from classical failure criteria. The current comparative studies indicate that the existing classical failure criterion exhibits limited predictive ability with computational data.
KW - Carbon fiber reinforced polymer composites
KW - Failure envelope
KW - Matrix nonlinear behavior
KW - Virtual testing method
UR - http://www.scopus.com/inward/record.url?scp=85160516522&partnerID=8YFLogxK
U2 - 10.1016/j.jmrt.2023.05.123
DO - 10.1016/j.jmrt.2023.05.123
M3 - Article
AN - SCOPUS:85160516522
SN - 2238-7854
VL - 24
SP - 8924
EP - 8939
JO - Journal of Materials Research and Technology
JF - Journal of Materials Research and Technology
ER -