• Jogi, Subhan Ali
• Baloch, Muhammad Moazam
• Chandio, Ghulaqm Sarwar
• Memon, I. A.

Abstract

In hybridization different fibers are stacked layer by layer to produce laminates have specific strength and stiffness and employed in light weight high strength applications.Physically mean fabricated hybrid composites used in aerospace, under water, body armors and armed forces establishment.In present work drop-weight impact response of hybrid composites were investigated by making laminates of hybrid composites.In Hybridization layers of E-glass (roving) and Kevlar 49 fabrics stacked with epoxy resin.The layers formulation was set up by hand layup method.Impregnationsof epoxy resin of commercial grade (601A) in fabrics were accomplished by VRTM (Vacuum Bagging Resin Transfer Molding) technique.Layup placementof Glass fibers/ Kevlar at 0°/90°, 45°/45° and 30°/60° were set for this work.Mechanical properties such as impact strength, bear resistance and break resistance were analyzed by usingASTM D-256 and D-3763 standard.Experimental investigation was conducted using instrumented Dart impact and Izod Impact test.E-glass/Kevlar 49 at layup 0°/90°and 30°/60°exhibited improvedimpact strength than 45°/45°.The surface morphology and fractography were also investigated by capturing different images of Specimens by using the SEM (Scanning Electron Microscopy).The fiberreinforcement and matrix fracture were also observed by using SEM.The SEM images suggest that epoxy resin tightly bonded with Kevlar fibers whereas Glass fibers were pulled out from laminations.

Topics

• surface
• scanning electron microscopy
• glass
• glass
• strength
• composite
• impact test
• resin
• fractography
• impact response