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Advances in Materials Science and Engineering
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Advances in Materials Science and Engineering
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2018
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Article
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Fig 7
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Research Article
Mode-I Metal-Composite Interface Fracture Testing for Fibre Metal Laminates
Figure 7
Load-displacement curve of C-C configuration for different cohesive element sizes: (a)
= 1 mm, (b)
= 0.5 mm, and (c)
= 0.3 mm.
(a)
(b)
(c)