Numerical and experimental study of multimode failure phenomena in GFRP laminates of different lay-ups
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...Gupta et al.([34]) found that for delamination characterization in a GF/EP laminate, stiffness value of 10(6) N/mm(3) and element size of 0....
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...and Gupta et al.([34]) concluded that maximum traction, interface shear strength, penalty shear stiffness, mesh/element size, viscosity parameter and fracture toughness are crucial factors for correct representation of load-displacement graph....
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...[44] Gupta et al.[34] found that for delamination characterization in a GF/EP laminate, stiffness value of 106 N/mm3 and element size of 0.25 and 0.125 are desirable, where layups are cross-ply, angle ply and quasi-isotropic in nature....
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...Numerical methods are also gaining wide acceptability for fracture characterization, for which tensile, compressive shear strength and fracture energies of the material([34]) need to be established....
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...Kharratzadeha et al.,[88] Johar,[91] Lu et al.[102] and Gupta et al.[34] concluded that maximum traction, interface shear strength, penalty shear stiffness, mesh/element size, viscosity parameter and fracture toughness are crucial factors for correct representation of load-displacement graph....
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...Cohesive zone element COH3D8 is used to model the interface between plies that break during impact loading resulting into delamination [18]....
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References
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"Numerical and experimental study of..." refers methods in this paper
...To get the length of cohesive zon,e different models are present, but the most commonly used model is Hillerborg's model [15,28]....
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...Puck failure criteria are used modelling matrix cracking [21,22]....
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