journal article·2010-09

Finite fracture mechanics analysis of crack onset at a stress concentration in a UD glass/epoxy composite in off-axis tension

J. Andersons, S. Tarasovs, E. Spārniņš

Composites Science and Technology· Volume 70· Issue 9
Publisher page

Abstract

The presence of stress concentrations at holes and notches is known to reduce the strength of composite materials. Due to complexity of the damage processes at a stress raiser in a composite, different modeling approaches have been developed, ranging from empirical point and average stress criteria to involved damage mechanics or cohesive zone-based models of failure. Finite fracture mechanics approach with a coupled stress and energy failure criterion, recently developed and applied mainly to cracking in homogeneous isotropic materials, allows predicting the appearance and propagation of a crack using material strength and toughness characteristics obtained from independent tests. The present study concerns application of the finite fracture mechanics to the analysis of cracking at a notch in a UD glass/epoxy composite subjected to tensile off-axis loading. Based on UD composite strength and intralaminar toughness characterized by separate tests, finite fracture mechanics analysis provided conservative estimates of crack onset stress at the notch.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Epoxy Resin Curing Processes · Structural Analysis of Composite Materials

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

References (54)

Show source-provided references
1. Characterization and analysis of delamination fracture in composites: an overview of developments from 1990 to 200110.1115/1.1504848 ↗
2. Dependence of fracture toughness of composite laminates on interface ply orientations and delamination growth direction10.1016/j.compscitech.2004.03.007 ↗
3. Interlaminar fracture of multidirectional glass/epoxy laminates under mixed-mode I+II loading10.1007/s11029-007-0023-1 ↗
4. Application of fracture mechanics to anisotropic plates10.1115/1.3607864 ↗
5. An energy release rate criterion for crack growth in unidirectional composite materials10.1016/0013-7944(89)90002-7 ↗
6. Strain energy release rates in finite graphite/epoxy plates with a crack under mixed mode deformation10.1177/073168449000900403 ↗
7. Suresh N, Wang ASD. Stress and energy based fracture conditions for fiber-wise splitting in composites. In: Composite materials: fatigue and fracture, vol. 5. ASTM STP 1230; 1995. p. 176–85.10.1520/STP14014S ↗
8. Stress fracture criteria for laminated composites containing stress concentrations10.1177/002199837400800303 ↗
9. Notched strength of composite laminates: predictions and experiments – a review10.1177/073168448500400102 ↗
10. Laminated composites containing an elliptical opening. I. Approximate stress analyses and fracture models10.1177/002199838702101004 ↗
11. Notch sensitivity and damage mechanisms of glass mat reinforced polypropylene10.1002/pc.10259 ↗
12. Strength of composite laminates containing holes and subjected to complex loading conditions10.1177/002199839703101203 ↗
13. Characterisation and modelling of the notched tensile fracture of woven quasi-isotropic GFRP laminates10.1016/S0266-3538(00)00238-4 ↗
14. An accurate method to predict the stress concentration in composite laminates with a circular hole under tensile loading10.1007/s11029-007-0033-z ↗
15. Laminated composites containing an elliptical opening. II. Experiment and model modification10.1177/002199838702101005 ↗
16. A progressive damage model for laminated composites containing stress concentrations10.1177/002199838702100904 ↗
17. Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings10.1177/002199839102500101 ↗
18. A progressive failure model for composite laminates containing openings10.1177/002199839102500505 ↗
19. A micro–macro approach to modeling progressive damage in composite structures10.1177/1056789506067941 ↗
20. Progressive failure analysis of composites10.1177/0021998308093912 ↗
21. Review of degradation models for progressive failure analysis of fiber reinforced polymer composites10.1115/1.3013822 ↗
22. Fracture analysis of notched composites10.1016/0045-7949(81)90119-X ↗
23. Tensile fracture of laminates with holes10.1177/002199838602000304 ↗
24. Tensile fracture of laminates with cracks10.1177/002199838602000305 ↗
25. Notch sensitivity of thermoset and thermoplastic laminates loaded in tension10.1007/BF01105690 ↗
26. In-plane shear failure analysis of notched composites10.1016/0266-3538(91)90003-8 ↗
27. An improved cohesive zone model for residual notched strength prediction of composite laminates with different orthotropic lay-ups10.1177/0021998304031635 ↗
28. Modelling of splitting and delamination in notched cross-ply laminates10.1016/S0266-3538(00)00170-6 ↗
29. Numerical investigation of progressive damage and the effect of layup in notched tensile tests10.1177/0021998305057432 ↗
30. The open hole tensile test: a challenge for virtual testing of composites10.1007/s10704-009-9333-8 ↗
31. A damage computational approach for composites: basic aspects and micromechanical relations10.1007/BF00356486 ↗
32. A mesomodel for localisation and damage computation in laminates10.1016/S0045-7825(99)00214-5 ↗
33. Prediction of size effects in notched laminates using continuum damage mechanics10.1016/j.compscitech.2007.02.005 ↗
34. A continuum damage model for composite laminates: part II – computational implementation and validation10.1016/j.mechmat.2007.03.006 ↗
35. Micromodel-based simulations for laminated composites10.1016/j.compscitech.2008.09.041 ↗
36. Strength or toughness? A criterion for crack onset at a notch10.1016/S0997-7538(01)01184-6 ↗
37. Quantized fracture mechanics10.1080/14786430412331280382 ↗
38. The fracture mechanics of finite crack extension10.1016/j.engfracmech.2004.07.001 ↗
39. Finite fracture mechanics: a coupled stress and energy failure criterion10.1016/j.engfracmech.2006.03.010 ↗
40. Taylor · 2007
41. A finite fracture mechanics approach to structures with sharp V-notches10.1016/j.engfracmech.2007.04.010 ↗
42. Numerical analysis of brittle crack initiation at stress concentrations in composites10.1080/15376490802135266 ↗
43. Finite thermoelastic fracture criterion with application to laminate cracking analysis10.1016/0022-5096(95)00080-1 ↗
44. Nairn JA. Applications of finite fracture mechanics for predicting fracture events in composites. In: Fifth international conference on deformation and fracture of composites, London; 1999. p. 10.
45. Transverse ply cracking in cross-ply CFRP laminates – initiation or propagation controlled?10.1177/002199839703101102 ↗
46. Initiation and growth criteria for transverse matrix cracks in composite laminates10.1016/S0266-3538(99)00114-1 ↗
47. Abe S, Kageyama K, Ohsawa I, Kanai M, Kato T. Analytical prediction and experiment of transverse lamina cracking in multidirectionally reinforced symmetric laminates. In: Proc of seventh Japan international SAMPE symposium and exhibition; 2001. p. 817–20.
48. Progressive cracking mastercurves of the transverse ply in a laminate10.1002/pc.20674 ↗
49. A fatigue failure criterion for fiber reinforced materials10.1177/002199837300700404 ↗
50. Static and fatigue strength of unidirectional composites under the combined effect of shear stress and transverse tension–compression stresses10.1007/BF00608850 ↗
51. Modeling the nonlinear deformation of composite laminates based on plasticity theory10.1007/s11029-007-0020-4 ↗
52. The onset of mixed mode intralaminar cracking in a cross-ply composite laminate10.1007/s11029-009-9055-z ↗
53. Micromechanical model of cross-over fibre bridging – Prediction of mixed mode bridging laws10.1016/j.mechmat.2007.07.007 ↗
54. A twofold strength and toughness criterion for the onset of free-edge shear delamination in angle-ply laminates10.1016/j.ijsolstr.2010.01.018 ↗