Abstract: The use of Composite material in aircraft industries is booming now-a day to grab the advantage of high strength to weight ratio. These materials are used to build main components of aircraft like fuselage, panels, rudder, and skins. It is unavoidable to provide different size, shaped cu touts in such components for different purpose i.e., inspection, maintenance. The deformed behaviour on composite plate with different loading conditions has been explored by many researchers in last 2 decades. The presented project is an attempt to summarize the issue of critically examines the current status, problems and opportunities to use of composite in aircraft industries. The loading on the fiber and the behaviour of the fiber orientation due to that loading condition is studied and upon that best orientation is decided i.e.., stacking orientation [0,90]S.
Keywords: Fiber orientation, Epoxy resin composites, Glass fiber, laminated polymer composites.
Title: Progressive Damage Analysis on Tensile and Flexural Strength of E-Glass Epoxy Laminates by Using Abaqus
Author: Hosamani Vijayavardhan Reddy
International Journal of Mechanical and Industrial Technology
ISSN 2348-7593 (Online)
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