Abstract
A Glass Aluminum fiber metal laminate GLARE is a set of materials manufactured by strong bonding glass/epoxy layers within the metal layers. The combined set of materials will be providing the better mechanical properties and weight reduction for an aircraft structure. The fiber metal laminate model was fabricated as per ASTM standards 200×30×5mm and then the experimental test under tensile loading test was conducted by using universal testing machine UTM as observed the stress-strain curve as the failure strength of GLARE reaching point and finally obtained results. Also to determine the mechanical properties and material characteristics of the unidirectional loading on E-glass fibers used to assemble GLARE for an aircraft structure.
Highlights
The history of the aerospace industry and aviation, have been conducting intense research work on various types of materials that have been conducted
The significant approach of materials under evaluation for major and minor aircraft structure components are in GLARE laminate, a sandwich material assemble from alternating layers of an aluminum and E- Glass fiber material with the bond layer
The reviewed works of a literature study of GLARE composite application in advance aerospace structures domain was extremely focused on the support of research
Summary
The history of the aerospace industry and aviation, have been conducting intense research work on various types of materials that have been conducted. The latest trend of material like FMLs will be providing the opportunity to use the combined laminate of aluminum with glass/epoxy composite. Aircraft manufacturers from all over the worldwide are incorporating the material in use and evaluating materials performance that can save weight. The significant approach of materials under evaluation for major and minor aircraft structure components are in GLARE laminate, a sandwich material assemble from alternating layers of an aluminum and E- Glass fiber material with the bond layer. According to relevant works of literature, the material takes a joined benefit of the high stiffness and high strength, better yielding properties, better resisting of thermal conducted material and low density form of aluminum panel sheets and the rupture resistance of the glass fibers.
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