journal article·2003-08

Analysis of specimen thickness effect on interlaminar fracture toughness of fibre composites using finite element models

Arun Agrawal, P.-Y. Ben Jar

Composites Science and Technology· Volume 63· Issue 10
Publisher page

Abstract

Abstract This work investigated accuracy of various mathematical expressions used to calculate the critical strain energy release rate (Gc) for delamination in fibre composites. Three mathematical expressions were considered here, based on (i) a simple beam theory, (ii) a transverse shear deformation theory, or (iii) a corrected beam theory with consideration of transverse shear deformation and crack tip singularity. Variable selected to examine accuracy of these expressions was specimen thickness. Since Gc is a material property, change of specimen thickness should not affect its value. The study used 2-dimensional finite element models with a blunt starting defect, which have length and geometry simulating the test coupons used for the delamination tests. For delamination in the shear mode (Mode II), we assumed that contact surfaces along the starting defect were free from friction, in order to be consistent with the beam theory expressions used for the calculation of Gc. As the finite element analysis used is static in nature, only the strain energy release rate for crack initiation was examined. The study firstly assigned a constant load of 1 N for the 10 mm-thick models, and then calculated the corresponding loads for models of other thickness based on constant strain energy release rates, GI and GII for Mode I (tension mode) and Mode II respectively, using the three beam theory expressions. For each model under the given load, stresses in the vicinity of the starting defect were then examined to determine whether the specimen thickness affects the stress values. Stresses used were the maximum principle stress and the von Mises stress along the contour of the starting defect, and the normal stress and shear stress along the boundary of the interlaminar resin-rich region, which were treated as the stress criteria for fracture initiation. The study concludes that the corrected beam theory provides Gc expressions that are least sensitive to the specimen thickness in both deformation modes.
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Research context

OpenAlex topics: Mechanical Behavior of Composites · Mechanical stress and fatigue analysis · Fiber-reinforced polymer composites

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References (33)

Show source-provided references
1. Standard test method for mode-I interlaminar fracture toughness of unidirectional fibre reinforced polymer matrix composites. ASTM Standard D 5528-94a, DCB standard, ASTM annual book of standards, 1999. Vol. 15.03: ASTM; 1999.
2. Protocols for interlaminar fracture testing of composites: European structural integrity society. Delft, Netherlands, 1993.
3. Testing methods for interlaminar fracture toughness of carbon fibre reinforced plastics, JIS K 7086: Japan Industrial Standards Group, Tokyo, Japan; 1993.
4. Mode II stress-intensity factors for cracked wood beams10.1016/0013-7944(77)90029-7 ↗
5. Prestandardization study on mode II interlaminar fracture toughness test for CFRP in Japan10.1016/0010-4361(95)93669-B ↗
6. O'Brien TK. Composite interlaminar shear fracture toughness, GIIc: shear measurement or sheer myth? In: Bucinell RB, editor. Composite materials: fatigue and fracture, Vol. 7th. ASTM STP 1330: ASTM, 1998. p. 3–18.
7. Standard test methods for delamination resistance of composites materials10.1023/A:1008869811626 ↗
8. Mode II delamination failure mechanisms of polymer matrix composites10.1023/A:1018552506085 ↗
9. Davies P, Ducept F, Brunner AJ, Blackman BRK, de Morais AB. Development of a standard mode II shear fracture test procedure. Seventh European Conference on Comp Mater, vol. 2, London: May 1996. p. 9–15.
10. Comparison of test configuration for determination of mode II interlaminar fracture toughness results from international collaborative test programme10.1179/146580199101540600 ↗
11. Interlaminar fracture toughness10.1016/S1359-8368(97)00013-9 ↗
12. Mode-II Interlaminar Fracture of Composites
13. Factors affecting the interlaminar fracture energy of graphite/epoxy laminates
14. Daniel · 1994
15. On the analysis and design of the end notched flexure (ENF) specimen for mode II testing10.1177/002199838602000606 ↗
16. The fracture mechanics of delamination tests10.1243/03093247V244207 ↗
17. The mixed-mode delamination of fibre composite materials10.1016/0266-3538(93)90031-B ↗
18. End corrections for crthotropic DCB specimens10.1016/0266-3538(89)90058-4 ↗
19. The analysis of interlaminar fracture in uniaxial fibre-polymer composites10.1098/rspa.1990.0007 ↗
20. Corrections for mode II fracture toughness specimens of composite materials10.1016/0266-3538(92)90096-L ↗
21. The effect of geometry, rate and temperature on mode I, mode II, and mixed-mode I/II interlaminar fracture of carbon-fibre/poly(ether-ether ketone) composites10.1177/002199839002400902 ↗
22. On the analysis of the end-notched flexure specimen for measuring the mode II fracture toughness of composite materials10.1016/0266-3538(94)90142-2 ↗
23. Round-robin interlaminar fracture testing of carbon-fibre-reinforced epoxy and PEEK composites10.1016/0266-3538(92)90003-L ↗
24. Influence of ENF Specimen geometry and friction on the mode II delamination resistance of carbon/PEEK10.1177/089270579701000404 ↗
25. The influence of loading rate on the mode II interlaminar fracture toughness of composite materials10.1177/002199839703101401 ↗
26. ANSYS. Online ANSYS user manual, Version 5.7, ANSYS Inc, Canonsburg, PA, USA.
27. Study of mode-I interlaminar crack growth in specimens of fibre-reinforced composites10.1016/S0266-3538(97)00102-4 ↗
28. Initiation of a mode-II interlaminar crack from an insert film in the end-notched flexure composite specimen10.1016/S0266-3538(99)00119-0 ↗
29. Finite element analysis of ENF specimen for measuring mode II fracture toughness10.1016/0266-3538(86)90031-X ↗
30. Strain energy release rate analysis of the ENF specimen using the finite element method10.1520/CTR10275J ↗
31. Finite element analysis of ENF specimens10.1520/CTR10322J ↗
32. Finite element analysis of beam specimens used to measure the delamination resistance of composites10.1520/CTR10104J ↗
33. A Finite element calculation of stress intensity factors by a modified crack closure integral10.1016/0013-7944(77)90013-3 ↗