AN EXPERIMENTAL INVESTIGATION ON GLASS EPOXY RESIN AND CARBON EPOXY RESINS FOR AEROSPACE APPLICATIONS

DOI: https://doie.org/10.1213/Jbse.2024988849

Syed Siraj Ahmed Ahmed Pasha, Dr. Swamy R. P,

Keywords:

Resin, laminates, glass, carbon fiber, tufted structures, aircraft, and compression strength

Abstract:

With a 10:1 resin to hardener ratio, the goal of this research is to create laminates employing glass and carbon fiber. The study looks at the processes involved in designing tufted structures for aircraft, including material selection, manufacturing processes, and mechanical testing. Tufting technology enhances interlaminar resistance to delamination, according to the results. Tensile strength is maximum for the EWM laminate without tufting, and compression and bending strength are highest for glass fiber tufted at a 45-degree angle. 

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