• Manjeet Singh
• Arjun
• Vishaldeep

Present work deal with the the S-glass/epoxy and carbon/epoxy laminate which are used to compare the tensile strength and elastic strain of the plate individually. The simulation is done in the Ansys workbench software of the composite plate. All the parameter are specified in the examination and concluded some results like the maximum stress of carbon epoxy plate is 14.298 MPa and maximum stress of S-glass epoxy plate is 14.065 MPa and maximum strain in carbon epoxy plate is .0016487mm and maximum strain in S-glass epoxy laminate plate is 0.0016797mm. From these results the carbon epoxy plate with hole geometry has higher tensile strength as compare to S-glass epoxy plate with hole geometry under the same circumstances also the strain is little bit lower than the S-glass epoxy plate compare to carbon epoxy plate.

Composite laminate, Tensile strength, ANSYS, Carbon Epoxy.

"Finite Element Method in composite laminates for tensile/bending test", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 3, page no.968-979, March-2019, Available :http://www.jetir.org/papers/JETIREL06149.pdf

"Finite Element Method in composite laminates for tensile/bending test", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 3, page no. pp968-979, March-2019, Available at : http://www.jetir.org/papers/JETIREL06149.pdf