Experimental Investigation and Comparison of Fatigue Behavior of E-Glass, Corbon Fiber and Jute Fiber Reinforced Polymer Matrix Composite used as Implants

Abstract

This research paper constitutes the Fatigue behavior of E-glass fiber corbon and jute fibre reinforced polymer composite and study of 10% weight fraction E-glass fiber corbon and jute fibre reinforced polymer composite fabricated by using Hand Layup fabrication technique According to the ASTM Standard Fatigue test was conducted ie ASTM D3479 / D3479M-19 and ASTM D-3039 Standard the specimen is fabricated by using the Epoxy resin-LY556 as the matrix material and the Hardener-HY 951 with the 10% E-glass fiber corbon and jute fibre as the reinforcement material with fiber weight fraction, 0+/-90 0 fiber orientation. By using the Hand Layup fabrication technique the specimens are prepared and the fatigue tests conducted on E-glass fiber, carbon and jute fibre polymer composites fatigue strength evaluated. The tests are conducted under static tension and cyclic tension with mean fatigue stress equal to 10% of the E-glass fiber, corbon and jute fibre polymer composites tensile strength. The experimental results show the Gradually the cyclic load is applied for the 10% E-GFRP carbon and jute fibre Specimen, From the experimental results the cyclic load @40243 CYCLES with182.4MPa the E-Glass fibre polymer Composite at Failure ie 100% amount of E-Glass fibre cracks/delimitation takes place or fibre At Failure. Similarly Jute polymer Composite Fails at 23809 Cycles with 19.86 MPa and Carbon Fibre Composites Fails At 10 6 cyclic Load with1100 MPa and compare with human Tebia bone.