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Vibration Analysis of Carbon Fiber Reinforced Laminated Composite Skin with Glass Honeycomb Sandwich Beam Using HSDT
Subramani M, Arumugam A.B,
Published in Periodica Polytechnica Budapest University of Technology and Economics
2017
Volume: 61
   
Issue: 3
Pages: 213 - 224
Abstract
In this paper, the vibration analysis of uniform laminated composite sandwich beam with a viscoelastic core was studied. The governing equation of motion of the laminated composite sandwich beam has been derived based on higher order shear deformation theory (HSDT) in finite element model (FEM). The developed finite element model has been validated in terms of natural frequencies with the experimental values and the available literature. Various parametric studies have been performed to examine the impact of the core thickness, ply orientation and aspect ratio of the uniform laminated composite sandwich beam in response to free vibration for various boundary conditions. From the results it was concluded that that natural frequencies could be increased with increasing the core thickness and decreased with increasing the aspect ratio.
About the journal
JournalPeriodica Polytechnica Mechanical Engineering
PublisherPeriodica Polytechnica Budapest University of Technology and Economics
ISSN0324-6051
Open AccessYes