Proposition of a framework for the development of a cohesive zone model adapted to Carbon-Fiber Reinforced Plastic laminated composites

2013 ◽  
Vol 105 ◽  
pp. 199-206 ◽  
Author(s):  
T. Vandellos ◽  
C. Huchette ◽  
N. Carrère
2019 ◽  
Vol 54 (3) ◽  
pp. 163-175 ◽  
Author(s):  
Xiangyang Huang ◽  
Mengcheng Zhang ◽  
Chunsheng Song ◽  
Zude Zhou

The mutual orthogonality of components is inevitable in the three-dimensional structure of modern aircrafts and satellites. Taking the connection of the frame, stiffening rib and other ribs with the skin as an example, it can be simplified as L-shaped adhesive joints. This article analyzes to obtain the mapping relational model between the change in strain distribution and the evolution of adhesive damage in the adhesive area of straight carbon fiber–reinforced plastic plate for L-shaped carbon fiber–reinforced plastic adhesive joints based on the cohesive zone model in the ABAQUS software; determines the experimental layout of the distributed fiber Bragg grating sensors based on the simulation and analysis results; and embeds the fiber Bragg grating sensors into the straight carbon fiber–reinforced plastic adhesive parts, to demonstrate the mapping relational model between the change in strain distribution and the evolution of adhesive damage for carbon fiber–reinforced plastic adhesive parts obtained through previous simulation analysis by monitoring the cohesive zone damage of L-shaped adhesive joints. The maximum error between experimental results and simulation results does not exceed 8.5%. Finally, it monitors the cohesive zone damage of adhesive layer for L-shaped carbon fiber–reinforced plastic adhesive joints based on the fiber Bragg grating sensor from the perspective of the theory and experiment.


Materials ◽  
2021 ◽  
Vol 14 (3) ◽  
pp. 576
Author(s):  
Liang Luo ◽  
Jie Lai ◽  
Jun Shi ◽  
Guorui Sun ◽  
Jie Huang ◽  
...  

This paper investigates the working performance of reinforcement concrete (RC) beams strengthened by Carbon-Fiber-Reinforced Plastic (CFRP) with different anchoring under bending moment, based on the structural stressing state theory. The measured strain values of concrete and Carbon-Fiber-Reinforced Plastic (CFRP) sheet are modeled as generalized strain energy density (GSED), to characterize the RC beams’ stressing state. Then the Mann–Kendall (M–K) criterion is applied to distinguish the characteristic loads of structural stressing state from the curve, updating the definition of structural failure load. In addition, for tested specimens with middle anchorage and end anchorage, the torsion applied on the anchoring device and the deformation width of anchoring device are respectively set parameters to analyze their effects on the reinforcement performance of CFRP sheet through comparing the strain distribution pattern of CFRP. Finally, in order to further explore the strain distribution of the cross-section and analyze the stressing-state characteristics of the RC beam, the numerical shape function (NSF) method is proposed to reasonably expand the limited strain data. The research results provide a new angle of view to conduct structural analysis and a reference to the improvement of reinforcement effect of CFRP.


2021 ◽  
pp. 073168442098359
Author(s):  
Luyao Xu ◽  
Jiuru Lu ◽  
Kangmei Li ◽  
Jun Hu

In this article, a micro-heterogeneous material simulation model with carbon fiber and resin phase about laser ablation on carbon fiber reinforced plastic (CFRP) is established by Ansys. The ablation process of CFRP by nanosecond ultraviolet laser is simulated, and the mechanism of pulse energy and spot spacing on the heat-affected zone (HAZ) is studied, then the process parameters are optimized with the goal of HAZ size and processing efficiency, and finally the validity of the model is verified by experiments. It is found that the residual gradient and the width of the radial HAZ increase with the increase of the spot spacing, and the width of the axial HAZ decreases slightly with the increase of the spot spacing, which indicates the existence of the optimal spot spacing. Second, the ablation depth increases with the increase of the pulse energy, and the carbon fiber retains a relatively complete degree of exposure when the pulse energy is low, which has a certain guiding significance for the cleaning and bonding of CFRP.


2012 ◽  
Vol 42 (1) ◽  
pp. 55-70 ◽  
Author(s):  
A. Kasimzade ◽  
S. Tuhta

Analytical, Numerical and Experimental Examination of Reinforced Composites Beams Covered with Carbon Fiber Reinforced PlasticIn the article, analytical, numerical (Finite Element Method) and experimental investigation results of beam that was strengthened with fiber reinforced plastic-FRP composite has been given as comparative, the effect of FRP wrapping number to the maximum load and moment capacity has been evaluated depending on this results. Carbon FRP qualitative dependences have been occurred between wrapping number and beam load and moment capacity for repair-strengthen the reinforced concrete beams with carbon fiber. Shown possibilities of application traditional known analysis programs, for the analysis of Carbon Fiber Reinforced Plastic (CFRP) strengthened structures.


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