Paper Contents
Abstract
GFRP was prepared under ASTM E23 Standards. The impact behavior of an aluminiumglassepoxy fiber metal laminate Specimens were tested in the Impact (Izod Test) testing machine then Experimental results were Obtained. The Experimental results obtained show that the increasing of GFRP layers will influences the impact strength of the composite. The Numerical simulation also done by using ANSYS Software with the help of ACP Pre post and Transient Structural Analysis Method. To validate the proposed numerical model, a comparative evaluation between the results obtained from the model and experimental once was carried out. The FML has been widely used in aerospace industries and wind turbine blade for their good strength with low density.
Copyright
Copyright © 2024 I KATHIRAVAN. This is an open access article distributed under the Creative Commons Attribution License.
