Mixed-mode I + III interlaminar fracture of carbon/epoxy laminates
A new test was developed for measuring the mixed-mode I + III interlaminar fracture toughness. The specimen adopted was an 8-point bending plate (8PBP) with a cross-ply lay-up and a mid-thickness edge pre-delamination at the standard 0/0 interface. Finite element analyses (FEA) showed that a wide ra...
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Veröffentlicht in: | Composites. Part A, Applied science and manufacturing Applied science and manufacturing, 2009-04, Vol.40 (4), p.518-523 |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | A new test was developed for measuring the mixed-mode I
+
III interlaminar fracture toughness. The specimen adopted was an 8-point bending plate (8PBP) with a cross-ply lay-up and a mid-thickness edge pre-delamination at the standard 0/0 interface. Finite element analyses (FEA) showed that a wide range of mode mix ratios can be achieved by varying the load point displacements imposed. However, the need of FEA based experimental data reduction and of a relatively complicated fixture are important drawbacks of test developed. Nevertheless, results for carbon/epoxy laminates showed a realistic evolution of initiation
G
c values with the
G
III/
G mode mix ratio. |
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ISSN: | 1359-835X 1878-5840 |
DOI: | 10.1016/j.compositesa.2009.02.003 |