Abstract
This paper presents an experimental and numerical study focused on the tensile fibre fracture toughness characterisation of hybrid plain weave composite laminates using non-standardized Overheight Compact Tension (OCT) specimens. The position as well as the strain field ahead of the crack tip in the specimens was determined using a digital speckle photogrammetry system. The limitation on the applicability of standard data reduction schemes for the determination of the intralaminar fibre fracture toughness of composites is presented and discussed. A methodology based on the numerical evaluation of the strain energy release rate using the J-integral method is proposed to derive new geometric correction functions for the determination of stress intensity factor for alternative composite specimen geometries. A comparison between different methods currently available to compute the intralaminar fracture toughness in composites is also presented and discussed. Good agreement between numerical and experimental results using the proposed methodology was obtained.
| Original language | English |
|---|---|
| Title of host publication | 16th ICCM International Conference on Composite Materials |
| Place of Publication | Kyoto, japan |
| Publisher | International Committee on Composite Materials |
| Number of pages | 7 |
| Publication status | Published - 2007 |
Bibliographical note
16th ICCM International Conference on Composite MaterialsKyoto, Japan
08 -13 Jul 2007
Keywords
- Composites Finite elements Fracture mechanics Fracture toughness Composite materials Crack tips Finite element method Geometry Glass ceramics Laminated composites Numerical methods Paper laminates Photogrammetry Strain energy Strain rate Compact tension Composite laminate Composite specimens Experimental and numerical studies Geometric correction Intralaminar fracture toughness J-integral method Specimen geometry
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