Published Paper Details:

Carbon Fiber Reinforced Polymer (CFRP) Composite Materials are Comes Under the Advanced Class Composite Materials, Are Commonly Preferred in Strategic Applications. However, the brittleness, air bubbles formed during the preparing of reinforcement resin, crack-prone matrix, and Fiber-matrix interface with a weak adhesion usually contribute to the failure of composite structures in terms of delamination and catastrophic failure. So, in the current work, Epoxy matrix CFRP composites are made using a hand lay-up process with varied amounts of Graphene Oxide (GO) (0%,0.25%,0.5%, and 1%) as a Nano Filler with Epoxy Polymer and nearly 90% of air bubbles are removed with the help of vacuum pump and desiccator. The samples will be Prepared According to the ASTM Standards and Tested Under Tension and 3 Point Bending Conditions. The maximum tensile strength, maximum flexural strength of 866.67MPa and 761.22MPa were observed for the 0.25%, 1% GO reinforced composites respectively.