Jianwen Bao

Abstract: This paper was aimed to investigate the hygrothermal effects on the mechanical behavior of the double lap shear joints of Carbon/Epoxy composite laminates, which were bonded using epoxy adhesive film SY14. First, experimental method was used to evaluate the hygrothermal dependent properties of the adhesive and the static response of composite laminate double lap joints at various environment conditions. The specimens were grouped into room temperature/dry (RD), room temperature/wet (RW), elevated temperature/dry (ED) and elevated temperature/wet (EW). The wet specimens were immersed in deionized water at temperature of 90 °C for 60 h and the elevated temperature is 95 °C. Tensile tests were carried out at room temperature and elevated temperature (95 °C) in a controlled chamber. Results showed that the elastic modulus and tensile strength decreased about 24% and 27% respectively after exposure to humidity environment. And a large degradation was found when exposure to high temperature while the plasticity became notable. The failure modes of the double lap shear joints were studied by visual inspection. It was found that both adhesive and cohesive failure happened for dry specimens at room temperature. While failure modes were dominated by cohesive failure after moisture exposure and adhesive failure at elevated temperature. Second, a finite element model was utilized to simulate the damage evolution of the double lap joints. The moisture diffusion process, swelling stress and thermal stress were included. And hygrothermal dependent cohesive law was considered to study the damage evolution. It revealed that failure modes were highly dependent on the weaker strength of adhesive and cohesive. Moisture absorption caused large degradation in cohesive strength, so the failure modes were mostly cohesive failure. Elevated temperature decreases strength of adhesive seriously, so adhesive failure dominates. Good agreement was achieved between the predicted failure loads and experimental results. And the predicted failure modes were also consistent with the experimental phenomenon.

TL;DR: In this paper, a 3D progressive finite element model was established to simulate scarf repaired laminates subjected to low velocity impact, in which intralaminar damage evolution was captured by user-defined subroutine and interlaminar delamination was simulated via the failure of zero-thickness cohesive elements inserted between plies.

TL;DR: In this paper, the impact performance of scarf-repaired composite laminates was investigated by experimental and numerical methods using continuum damage mechanics and cohesive elements were used in all the interfaces of the adherends (i.e. the patch and the parent).

TL;DR: In this paper, the properties of two types of adhesives from the same material system, SY14M (an elevated temperature curing epoxy adhesive) and SY24C (a medium temperature cured epoxy glue), were studied in different environment conditions, and an adhesive selection method based on property matching between adhesive tensile and shear strength was proposed.

TL;DR: In this article, a finite element model was developed to simulate the failure process and predict structural strength, in which moisture diffusion, hygrothermal stress analysis and progressive damage model were considered.