Journal
COMPOSITE STRUCTURES
Volume 293, Issue -, Pages -Publisher
ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2022.115730
Keywords
Composite laminate; Progressive failure; Phase field model; Effective strain variables; Explicit scheme
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Funding
- National Natural Science Foundation of China [12172079]
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Fiber reinforced composites have complex failure mechanisms that are challenging to simulate accurately. This paper presents a double-phase field model that characterizes fiber damage and matrix damage using two different phase fields. The failure mechanisms are identified through a new strain energy density form and effective constitutive tensor. The proposed model embeds specified damage initiation and evolution criteria by coupling with redefined degradation functions. The model is implemented in an explicit manner and verified through experimental comparisons.
Fiber reinforced composites have very excellent mechanical properties due to their sophistic microstructures. At the same time these microstructures can induce complex failure mechanisms including intralaminar damage, interlaminar damage and the interactions between them. Nevertheless, high fidelity simulations for these complex failure mechanisms are still challenging. In this paper, we develop a double-phase field model for complex failure in fiber reinforced composite. In the model, two different phase fields, i.e., fiber phase field and matrix phase field, are adopted for characterizing fiber damage and matrix damage, respectively. The failure mechanisms of fiber damage as well as the other modes in matrix damage are identified through a new strain energy density form that contains four different effective strain variables as well as a new effective constitutive tensor. Then by coupling with redefined degradation functions corresponding to different failure mechanisms, specified damage initiation and evolution criteria can be embedded into the proposed model automatically. Moreover, the new model is implemented in an explicit manner. The proposed model is verified and validated through the comparison between the predicted results and that of the experiments on the failure in unidirectional block and composite laminate.
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