Published October 2017 | Version v1
Journal article

Evaluation of impact strength of epoxy based hybrid composites reinforced with e-glass/kevlar 49

  • 1. Dawood University of Engineering and Technology, Karachi (Pakistan). Dept. of Metallurgy and Material Engineering
  • 2. Mehran University of Engineering and Technology, Jamshoro (Pakistan). Dept. of Metallurgy and Material Engineering
  • 3. NED University of Engineering and Technology, Karachi (Pakistan). Dept. of Metalurgical Engineering

Description

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. Impregnations of 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 degree/90 degree, 45 degree/45 degree and 30 degree/60 degree were set for this work. Mechanical properties such as impact strength, bear resistance and break resistance were analyzed by using ASTM 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 degree/90 degree and 30 degree/60 degree exhibited improvedimpact strength than 45 degree/45 degree. 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. (author)

Additional details

Publishing Information

Journal Title
Mehran University Research Journal of Engineering and Technology
Journal Volume
36
Journal Issue
4
Journal Page Range
p. 1009-1016
ISSN
0254-7821