journal article·2006-08

A non-classical, energy release rate based approach for predicting delamination growth in graphite reinforced laminated polymeric composites

Barry D. Davidson, Ryan D. Bialaszewski, Satish S. Sainath

Composites Science and Technology· Volume 66· Issue 10
Publisher page

Abstract

Abstract A non-classical, energy release rate based approach is applied to predict delamination growth in four different graphite reinforced laminated polymeric matrix composites, and the results are compared to those obtained using classical, linear elastic fracture mechanics. Both methods predict delamination advance by comparing the energy release rate in a structure to its critical value, or toughness, where the toughness is obtained from a series of tests on unidirectional laminates with midplane delaminations. However, the non-classical method uses a “crack tip element/non-singular field” approach to decompose the energy release rate, which results in non-classical mode I and mode II components. Matrix materials considered include an epoxy, a blended thermoplastic toughened epoxy, a thermoplastic particulate interlayer toughened epoxy, and a thermoplastic. For all materials, the non-classical approach is shown to provide relatively accurate predictions, whereas relatively poor results are obtained when using the classical approach. In view of the range of materials studied, it is concluded that the non-classical approach will likely apply to other current and future generation graphite reinforced polymeric matrix composites, and that this approach will continue to give more accurate results than one that is classically based.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Structural Behavior of Reinforced Concrete

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (35)

Show source-provided references
1. Evaluation of energy release rate-based approaches for predicting delamination growth in laminated composites10.1023/A:1007647226760 ↗
2. Accuracy assessment of the singular field-based mode mix decomposition procedure for the prediction of delamination
3. Mixed-mode fracture in fiber–polymer composite laminates
4. On the analysis of mixed-mode failure10.1007/BF00035361 ↗
5. The mixed-mode delamination of fibre composite materials10.1016/0266-3538(93)90031-B ↗
6. An analytical crack tip element for layered elastic structures10.1115/1.2895931 ↗
7. Micromechanisms of fracture in toughened graphite–epoxy laminates
8. Relating resin mechanical properties to composite delamination toughness10.1177/002199838902300904 ↗
9. DCB testing of thermoplastic composites: a non-linear micro–macro numerical analysis10.1016/S0266-3538(96)00166-2 ↗
10. Mode I and Mode II fracture toughness measured between differently oriented plies in graphite/epoxy composites
11. Effects of mode ratio, ply orientation and precracking on the delamination toughness of a laminated composite10.1177/073168449601500202 ↗
12. Beam analysis of angle-ply laminate mixed-mode bending specimens10.1016/S0266-3538(98)00128-6 ↗
13. Prediction of energy release rate for edge delamination using a crack tip element approach
14. A finite element calculation of stress intensity factors by a modified crack closure integral10.1016/0013-7944(77)90013-3 ↗
15. Convergence of strain energy release rate components for edge-delaminated composite laminates10.1016/0013-7944(88)90196-8 ↗
16. Development of TORAYCA Prepreg P2302 carbon fiber reinforced plastic for aircraft primary structural materials10.1163/156855196X00301 ↗
17. Mode I and Mode II delamination growth of interlayer toughened carbon/epoxy (T800H/3900-2) composite system
18. Whitney · 1987
19. Standard test method for mixed mode I–mode II interlaminar fracture toughness of unidirectional fiber reinforced polymer matrix composites, American Society for Testing and Materials Standard D6671; 2003.
20. Three dimensional analysis and resulting design recommendations for unidirectional and multidirectional end-notched flexure tests10.1177/002199839502901602 ↗
21. Three dimensional analysis of center delaminated unidirectional and multidirectional single leg bending specimens10.1016/0266-3538(95)00069-0 ↗
22. Evaluation of data reduction procedures for the mixed mode bending test10.2514/2.129 ↗
23. Effect of stacking sequence on delamination toughness and delamination growth behavior in composite end-notched flexure specimens
24. Interlaminar shear fracture toughness and fatigue thresholds for composite materials
25. Assessment of evaluation methods for the mixed-mode bending test10.1520/CTR10611J ↗
26. A mixed-mode failure criterion derived from tests on symmetric and asymmetric specimens10.1016/S0266-3538(98)00105-5 ↗
27. Crews Jr JH, Shivakumar KN, Raju IS. A fiber-resin micromechanics analysis of the delamination front in a DCB specimen, NASA Technical Memorandum 100540, January; 1988.
28. A three-dimensional crack tip element for energy release rate determination in layered elastic structures10.1177/002199801772662118 ↗
29. Energy release rate prediction in stiffened-skin structure using a three dimensional crack tip element analysis10.1177/0021998305051802 ↗
30. Analysis of instability-related delamination growth using a crack tip element10.2514/3.11900 ↗
31. Accuracy assessment of a three dimensional, crack tip element based approach for predicting delamination growth in stiffened-skin geometries10.1007/s10704-004-8155-y ↗
32. Nonlinear analysis of homogenous, symmetrically delaminated single leg bending specimens10.1520/CTR10849J ↗
33. A single leg bending test for interfacial fracture toughness determination10.1007/BF00034525 ↗
34. An unsymmetric end-notched flexure test for interfacial fracture toughness determination10.1016/S0013-7944(98)00017-4 ↗
35. Effects of friction, geometry and fixture compliance on the perceived toughness from three and four point bend end notched flexure tests10.1177/0731684405050402 ↗