Date of Publication :19th June 2019
Abstract: Laminated composites are made of layers of fibers in matrix material. They are very thin and light weight which makes them efficient in various applications. However, this thin configuration itself makes them prone to vibration damage. In this paper, an attempt has been made to study vibration response of laminated composite box beams. The variation of orthotropic stiffness parameter with natural frequency for different length to width ratios is studied. Analysis is based on finite element principles implemented via ANSYS 15
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