Abstract
Nowadays, the demand for carbon-boron boron-based composites has tremendously increased in the aerospace and automotive industries due to their lightweight and high strength-weight ratio. Hence, it is necessary to study the vibrational behavior of the carbon-boron matrix. The stacking sequences, fiber orientation, crack size, and length-width ratio has all been studied at three levels. A mathematical model has been developed using classical laminated plate theory to evaluate the natural frequency for two boundary conditions; first, all sides were supported (SSSS), second, two adjacent sides clamped, and the other two were simply supported (CCSS). Grey relation analysis has also been applied to optimize the parameters.
Publisher
AMG Transcend Association
Subject
Molecular Biology,Molecular Medicine,Biochemistry,Biotechnology
Cited by
2 articles.
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