Finite Element Analysis for Composite Laminates
ANSYS Composite Laminate FEA – Limited-Budget Research Assistance I am looking for an ANSYS specialist or postgraduate researcher experienced in composite…
Offer description
ANSYS Composite Laminate FEA – Limited-Budget Research Assistance I am looking for an ANSYS specialist or postgraduate researcher experienced in composite materials to perform a comparative finite element analysis of two carbon/epoxy composite laminates. Laminate specifications Plate dimensions: 200 mm × 100 mm Material: Carbon/Epoxy Number of plies: 8 Individual ply thickness: 0.2 mm Total thickness: 1.6 mm Density: 1600 kg/m³ Laminate A: [0/30/60/90]s Laminate B: [0/45/−45/90]s Material properties Longitudinal Young's modulus, E1 = 230 GPa Transverse Young's modulus, E2 = 23 GPa In-plane shear modulus, G12 = 9 GPa Through-thickness shear modulus, G23 = 8 GPa Major Poisson's ratio, ν12 = 0.2 Please identify any additional material properties ...
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