Coupled thermal-mechanical damage model of laminated carbon fiber/resin composite subjected to lightning strike. (15th December 2018)

• Record Type: Journal Article
• Authors: Dong, Qi; Wan, Guoshun; Ping, Lu; Guo, Yunli; Yi, Xiaosu; Jia, Yuxi
• Is Part Of: Composite structures. Volume 206(2018)
• Page Start: 185
• Page End: 193
• Publication Date: 2018-12-15
• Subjects: Carbon fibers -- Laminate mechanics -- Thermal ablation -- Lightning strike damage -- Finite element analysis (FEA); Composite construction -- Periodicals; Composites -- Périodiques; 624.18
• DOI: 10.1016/j.compstruct.2018.08.043
• Languages: English
• ISSNs: 0263-8223

Abstract

Abstract: The degradation model of stiffness matrix containing thermal-mechanical coupling damage was constructed by the user-defined subroutine VUMAT on the basis of continuum damage mechanics (CDM) and phenomenological analysis method, then, it was introduced to the software ABAQUS/Explicit to simulate the damage caused by lightning induced effects of thermal ablation and expansion on carbon fiber reinforced polymer (CFRP) laminates. The results revealed the evolution of the coupling damage from the analysis of stress-strain state and damage variables involved. It can be concluded that the thermal-mechanical coupling model pushed the simulated in-plane damage much closer to the experimental results than thermal ablation model, and the good consistency of simulated in-depth damage and experimental results indicated that the lightning induced in-depth damage was mainly brought from the combined impacts of thermal ablation and expansion.