Design and Analysis of Aluminium’s Sheet Delamination Repair Using Composite Materials

This abstract presents a Tensile approach for the repair of cracked aluminum structures through the integration of advanced composite materials, specifically epoxy carbon with a Young’s Modulus of 395 GPa, and a copper metal matrix composite (MMC) alloy. The study employs the ANSYS Static Structural analysis to evaluate the structural integrity and performance of the repaired aluminum components. The cracked aluminum structures are modeled, and the epoxy carbon composite is strategically applied to the damaged regions. Additionally, a copper MMC alloy is introduced to enhance the mechanical properties of the repaired sections. The ANSYS Static Structural analysis provides critical insights into stress distribution, deformation, and overall structural response, aiding in the optimization of the repair design. This innovative approach aims to extend the service life of aluminum structures by leveraging the synergistic benefits of epoxy carbon and copper MMC composites, demonstrating the potential for enhanced durability and performance in aerospace, automotive, and other engineering applications.