Published Paper Details:

Glass, Carbon and hybrid fiber material is a well-established branch of research in composite structures stability. It has a wide range of applications in engineering science and technology. Polymeric materials reinforced with synthetic fibers such as glass, carbon, and hybrid fiber provide advantages of high stiffness and strength to weight ratio as compared to conventional construction materials. Composite subjected to in-plane loads is an important consideration in the preliminary design of aircraft and launch vehicle components. The sizing of many structural subcomponents of these vehicles is often determined by stability constraints. The purpose of this project was to generate the experimental and analytical investigation, conducted to find out the mechanical properties. In analytical method, the different types of stress distributions were found out by using the ANSYS 12 software. In experimental method, the mechanical properties were found by using tensile test and flexural test in universal testing machine. Composite fiber Plates are extensively used as structural members in aircraft design. The Glass fiber, carbon fiber and hybrid materials behavior of such has always received much attention by researchers. These materials were used access in the case of fuselage, wings, windows and doors. In some cases composite materials are used to reduce the weight of the structure. In aerospace and many other applications these structural components are also made up of composite material to further reduce the weight of the structure. The outstanding mechanical properties of composite structures, such as durability and corrosion-resistance characteristics combined with low density, make it more attractive compared to conventional materials.