journal article·2008-10Open access

Experimental optimization of the impact energy absorption of epoxy–carbon laminates through controlled delamination

Alessandro Pegoretti, Ivan Cristelli, Claudio Migliaresi

Composites Science and Technology· Volume 68· Issue 13

Abstract

Abstract In this paper, the correlation between interlaminar fracture toughness and impact energy absorption for the fracture of epoxy–carbon laminates was studied. Carbon fibres–epoxy cross-ply prepreg layers were interleaved with thin (26 μm) poly(ethylene-terephthalate) (PET) films. Before the composite preparation, circular holes 1 mm in diameter were drilled in the PET films at several densities (from 0 up to 44 holes/cm 2 ) in order to selectively increase the interlaminar contact area between the epoxy–carbon laminae. In this way, the interlaminar contact area was gradually varied from 0%, corresponding to the case in which non-perforated PET films were used, up to 100% in the case of non-interleaved laminates. The Mode I interlaminar fracture toughness of the resulting laminates was determined according to the ASTM D-5528-01 standard test method on double cantilever beam (DCB) specimens. The critical values of the strain energy release rate determined at the point at which the load versus opening displacement curve becomes non-linear ( G IC,NL ) resulted to vary from 40 up to 260 J/m 2 , depending on the interlaminar contact area. All the laminates were then characterized by three point bending tests performed both under quasi-static (5 mm/min) and impact (2 m/s) loading conditions. The elastic modulus of the laminates resulted to be practically independent of the level of interlaminar adhesion, while the bending strength decreased as the interlaminar fracture toughness decreased. The total energy to fracture evaluated under impact conditions showed a non-monotonic correlation with the interlaminar fracture toughness, reaching a maximum level in correspondence of a G IC,NL value of about 60 J/m 2 . At the same time, the ductility index, i.e. the ratio between the propagation and the initiation energies, evaluated by instrumented Charpy impact tests, markedly increased as the interlaminar fracture toughness decreased.
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Research context

OpenAlex topics: Mechanical Behavior of Composites · Epoxy Resin Curing Processes · Fiber-reinforced polymer composites

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References (52)

Show source-provided references
1. Mallick · 1993
2. Review of low-velocity impact properties of composite materials10.1016/1359-835X(96)00074-7 ↗
3. An overview of the impact behavior of fibre-reinforced composites
4. Influence of delamination on impact damage in composite structures10.1016/j.compscitech.2004.12.032 ↗
5. Damage tolerance of a stitched carbon/epoxy laminate10.1016/S1359-835X(97)00063-8 ↗
6. Drop-weight impact damage tolerance of CFRP with rubber modified epoxy matrix10.1016/0010-4361(93)90018-4 ↗
7. Influence of processing method on the fracture toughness of thermoplastic-modified, carbon-fiber-reinforced epoxy composites10.1016/S0266-3538(98)00140-7 ↗
8. Toughening mechanisms in rubber-modified glass fiber/unsaturated polyester composites10.1002/pc.10394 ↗
9. Interlaminar fracture toughness improvement in composites with hyperbranched polymer modified resin10.1016/j.compscitech.2005.01.005 ↗
10. In the effect of stitching on mode-I delamination toughness of laminated composites10.1016/0266-3538(94)90103-1 ↗
11. Determination of Mode II delamination toughness of stitched laminated composites10.1016/0266-3538(95)00089-5 ↗
12. On the effects of stitching in CFRPs—I. Mode I delamination toughness10.1016/S0266-3538(97)00229-7 ↗
13. On the effects of stitching in CFRPs—II. Mode II delamination toughness10.1016/S0266-3538(97)00186-3 ↗
14. Thermal degradation of the mode I interlaminar fracture properties of stitched glass fibre vinyl ester composites10.1023/A:1004365521648 ↗
15. Mode II delamination toughness of z-pinned laminates10.1016/j.compscitech.2004.02.008 ↗
16. Delamination of Z-pinned carbon fibre reinforced laminates10.1016/j.compscitech.2004.12.018 ↗
17. Effect of interlayer modulus on fracture mode ratio for interleaved composite laminates10.1016/0013-7944(95)00016-O ↗
18. Interlayer toughening of resin transfer molding composites10.1016/S1359-835X(00)00088-9 ↗
19. Loading rate dependence of Mode II fracture behavior in interleaved carbon fibre/epoxy composite laminates10.1023/A:1012658114593 ↗
20. Effect of interleaved non-woven carbon tissue on interlaminar fracture toughness of laminated composites: Part I – Mode II10.1177/0021998302036018981 ↗
21. Effect of interleaved non-woven carbon tissue on interlaminar fracture toughness of laminated composites: Part II – Mode I10.1177/0021998302036018980 ↗
22. Effect of ionomer thickness on mode I interlaminar fracture toughness for ionomer toughened CFRP10.1016/S1359-835X(99)00023-8 ↗
23. Toughening of carbon fiber/epoxy composite by inserting polysulfone film to form morphology spectrum10.1016/j.polymer.2004.08.020 ↗
24. Mode II delamination and damage resistance of carbon/epoxy composite laminates interleaved with thermoplastic particles10.1177/0021998306063356 ↗
25. Improving impact resistance of carbon-fibre composites through interlaminar reinforcement10.1016/S1359-835X(02)00010-6 ↗
26. Kim · 1998
27. Interfacial mobility and its effect on interlaminar fracture toughness in glass-fibre-reinforced epoxy laminates10.1007/BF00355930 ↗
28. The effect of glass–resin interface strength on the impact strength of fiber reinforced plastics10.1002/pen.760180203 ↗
29. Influence of fiber–matrix adhesion on mechanical properties of graphite/epoxy composites: I. Tensile, flexure, and fatigue properties10.1177/073168449901801105 ↗
30. Fiber–matrix adhesion and its effect on composite mechanical properties: IV. Mode I and Mode II fracture toughness of graphite/epoxy composites10.1177/002199839202600701 ↗
31. Goan JC, Martin TW, Prescott R. The influence of interfacial bonding on the properties of carbon fiber composites. In: 28th Annual Technical Conference Reinforced Plastic Composites Institute; 1973: SPI.
32. On the relationship between impact energy and delamination area10.1007/BF02321362 ↗
33. Improving the fracture energy of carbon fiber reinforced plastics by delamination promoters10.1007/BF00738470 ↗
34. On fiber composites with intermittent interlaminar bonding
35. Increased fracture toughness of graphite–epoxy composites through intermittent interlaminar bonding10.1177/002199838001400306 ↗
36. Controlled energy dissipation in fibrous composites, I. Controlled delamination10.1002/pc.750080205 ↗
37. Optimizing energy absorption in multi-layered materials through controlled delamination10.1023/A:1004630230780 ↗
38. Delamination threshold loads for low velocity impact on composite laminates10.1016/S1359-835X(00)00061-0 ↗
39. Effects of stacking sequence on the impact resistance in composite laminates – Part 1: parametric study10.1016/S0263-8223(98)00036-1 ↗
40. Recovery of post-yielding deformations in semi-crystalline poly(ethylene-terephthalate)10.1016/S0032-3861(99)00333-X ↗
41. Mode II delamination
42. Modes I and II interlaminar fracture toughness and fatigue delamination of CF/epoxy laminates with self-same epoxy interleaf10.1016/j.ijfatigue.2006.02.004 ↗
43. Interlaminar fracture characterization for plain weave fabric composites10.1023/A:1016025232102 ↗
44. The influence of matrix chemical structure on the Mode I and II interlaminar fracture toughness of glass-fiber/epoxy composites10.1002/pc.10014 ↗
45. Fracture behavior of interleaved fiber resin composites10.1016/0266-3538(91)90054-S ↗
46. Changing the toughness of graphite fiber/resin based composites by changing their internal structure10.1016/S1359-8368(00)00008-1 ↗
47. Mechanical properties of carbon woven reinforced epoxy matrix composites. A study on the influence of matrix modification with polysulfone10.1002/pc.10439 ↗
48. Roles of interfaces between carbon fibers and epoxy matrix on interlaminar fracture toughness of composites10.1163/156855406775997079 ↗
49. Mode I and mode II delamination properties of glass/vinyl-ester composite toughened by particulate modified interlayers10.1016/S0266-3538(03)00162-3 ↗
50. Fiber–matrix adhesion and its effect on composite mechanical properties: II. Longitudinal (0°) and transverse (90°) tensile and flexure behavior of graphite/epoxy composites10.1177/002199839102500802 ↗
51. The effect of fibre–matrix interface strength on the impact and fracture properties of carbon-fibre-reinforced epoxy resin composites10.1088/0022-3727/6/5/314 ↗
52. Methods for improving the impact resistance of composite materials