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Experimental and numerical analysis of pinned-joints composite laminates: Effects of stacking sequences
Faculty
Science
Year:
2013
Type of Publication:
Article
Pages:
3353-3366
Authors:
Mahmoud, F. F, Khashaba, U. A, Sebaey, T. A, Selmy, A. I, Hamouda, R. M
DOI:
10.1177/0021998312464891
Journal:
JOURNAL OF COMPOSITE MATERIALS SAGE PUBLICATIONS LTD
Volume:
47
Research Area:
Materials Science
ISSN
ISI:000327378300001
Keywords :
Pinned-joints, finite element, stacking sequence, bearing strength, ultimate strength, bearing stiffness
Abstract:
The present study investigates the effect of stacking sequence on the failure loads (strength) and modes of pinned-joints glass-fiber reinforced epoxy composite laminates. Specimens with {[}0/90](2S), {[}15/-75](2S), {[}30/-60](2S) and {[}45/-45](2S) stacking sequences were investigated both experimentally and numerically. A series of ASTM tests were performed on unidirectional {[}8](0) glass-fiber reinforced epoxy composite laminate to determine the properties of the single lamina that was needed for the finite element analysis. A 3D progressive damage model was built with the aid of ABAQUS software, failure criteria and property degradation rules to simulate the problem. The results showed that the {[}0/90](2S) laminate has the highest ultimate strength. The minimum bearing and ultimate strength was observed for {[}30/-60](2S) laminate. Loading the specimens up to the ultimate value lead to shear-out failure mode for {[}0/90](2S), {[}15/-75](2S) and {[}30/-60](2S) stacking sequences, while specimens with {[}45/-45](2S) stacking sequence are characterized by bearing failure mode. The experimental and numerical results agree well with a maximum Euclidean error norm of 8.57\%.
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