Journal Article

Modeling Progressive Damage and Failure of Single-Lap Thin-Ply-Laminated Composite-Bolted Joint Using LaRC Failure Criterion

Wang, Yao, Zheng, Kaidong, Liu, Hao, Ji, Yundong, Li, Shuxin, Cao, Dongfeng, Wang, Xiangjiang, Hu, Haixiao

2022

Overview

Thin-ply composite failure modes also significantly differ from conventional ply composite failure modes, with the final failure mechanism switching from irregular progressive failure to direct fracture characterized by a uniform fracture with the reduction of the ply thickness. When open holes and bolt joints are involved, thin-ply-laminated composites exhibit more complex stress states, damage evolution, and failure modes. Compared to the experimental study of thin-ply-laminated composite-bolted joints, there are few reports about numerical analysis. In order to understand the damage evolution and failure mechanism of thin-ply-laminated composites jointed by single-lap bolt, a progressive damage model based on three-dimensional (3D) LaRC failure criterion combined with cohesive element is constructed. Through an energy-based damage evolution method, this model can capture some significant mechanical characteristics in thin-ply-laminated structures, such as the in situ effect, delamination inhibition, and fiber compressive kinking failure. The comparisons between the numerical predictions and experimental observations are made to verify the accuracy of the proposed model. It is found that the predicted stress-displacement curves, failure modes, damage morphologies, etc., are consistent with the experimental results, indicating that the presented progressive damage analysis method displays excellent accuracy. The predicted stress at the onset of delamination is 50% higher than that of the conventional thick materials, which is also consistent with experimental results. Moreover, the numerical model provides evidence that the microstructure of thin-ply-laminated composite performs better in uniformity, which is more conducive to inhibiting the intra-layer damage and the expansion of delamination damage between layers. This study on the damage inhibition mechanism of thin-ply provides a potential analytical tool for evaluating damage tolerance and bearing capabilities in thin-ply-laminated composite-bolted joints.

• Publisher: MDPI AG,MDPI
• Subject: Accuracy / Bolted joints / Braided composites / Comparative analysis / Composite materials / Crack propagation / Criteria / Damage assessment / Damage tolerance / Deformation / Delamination / Ductility / Evolution / Failure analysis / Failure mechanisms / Failure modes / Kinking / Laminar composites / Laminated materials / Laminates / Mathematical models / Mechanical properties / Numerical analysis / Numerical models / Numerical prediction / Scanning electron microscopy / Shear strength / Shear stress / Stress state / Tensile strength / Three dimensional models / Titanium alloys