Preprint Article Version 1 Preserved in Portico This version is not peer-reviewed

Experimental and Numerical Investigation of Prepreg-RTM Co-Curing Molding Composite Bolted T-joint under Bending Load

Version 1 : Received: 29 February 2024 / Approved: 29 February 2024 / Online: 29 February 2024 (10:59:29 CET)

A peer-reviewed article of this Preprint also exists.

Zhang, T.; Luo, Z.; Li, K.; Cheng, X. Experimental and Numerical Investigation of Prepreg-RTM Co-Curing Molding Composite Bolted T-Joint under Bending Load. Polymers 2024, 16, 1018. Zhang, T.; Luo, Z.; Li, K.; Cheng, X. Experimental and Numerical Investigation of Prepreg-RTM Co-Curing Molding Composite Bolted T-Joint under Bending Load. Polymers 2024, 16, 1018.

Abstract

A set of polymer composite bolted T-joints with novel configuration consisting of internal skeleton and external skin was fabricated using a prepreg-RTM co-curing molding process. Experiments were conducted to study their mechanical properties under bending load. A finite element model with a polymer resin area between the skin and skeleton was established and verified by the experimental results. Then, the damage propagation process and failure mechanism of the joint and the influence of three factors related to the layer characteristics of the skin and skeleton were investigated by the validated models. The results show that the bending stiffness and the yield limit load of the novel composite T-joint are 0.81 times and 1.65 times that of the 2A12 aluminum T-joint respectively, while at only 55.4% of its weight. The damage of the joint initiates within the resin area and leads to a degradation of the joint bending performances. The preferred stacking sequence of the skeleton is [0/+45/90/-45]ns when primarily subjected to bending loads. The decrease in bending performances is within 5% with the inclining angle of the skeleton less than 12 degrees. The more layers of 90° in the skin, the better bending performances of the joints, while the more layer of 0°, the poorer bending performances.

Keywords

polymer composites; T-joint; prepreg-RTM co-curing molding; bending performance; finite element analysis; failure analysis

Subject

Engineering, Aerospace Engineering

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