journal article·2007-03

Effects of nonlinear viscoelastic behaviour and loading rate on transverse cracking in CFRP laminates

The Hoang Nguyen, Denys Gamby

Composites Science and Technology· Volume 67· Issue 3-4
Publisher page

Abstract

Abstract The progressive multiplication of matrix transverse cracks in cross-ply laminates made of long carbon fibre reinforced polymer (CFRP) is addressed in this study. Monotonic tensile tests performed on [03/903]S laminates at 120 °C have shown a marked dependence of cracking development on loading rate. This paper aims to assess the impact of the material nonlinearity on the loading rate sensitivity of the damaging process. A “shear-lag” damage analysis, using the nonlinear correspondence principle and appropriate failure criteria, is carried out to numerically predict the cracking evolution. This work shows that, though important, the material nonlinearity of the undamaged material does not significantly enhance the loading rate sensitivity of the cracking process and it cannot explain alone the phenomenon. On the other hand, taking into account the loading rate dependence of the critical strength, together with the R-curve effect, which gives good predicted cracking curves, suggests that the observed rate effect pertains to the viscoelastic character of the damaged material in the process zone close to crack fronts.
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Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Behavior of Reinforced Concrete · Structural Response to Dynamic Loads

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References (27)

Show source-provided references
1. Modeling of time-dependent behaviour of deformation and transverse cracking in cross-ply laminates10.1163/15685510152546358 ↗
2. Time-dependent damage in carbon fibre-reinforced polymer composites10.1016/1359-835X(96)00073-5 ↗
3. Time-dependent matrix cracking in cross-ply laminates10.1016/0266-3538(90)90029-5 ↗
4. Lafarie-Frenot MC. Influence of strain rate and temperature on transverse ply cracking of CFRP laminates. In: The 10th European conference on composite materials (ECCM 10), Bruges, Belgique; 2002.
5. A damage evolution model for viscoelastic composite laminates10.1520/CTR10907J ↗
6. Nguyen TH, Lafarie-Frenot MC, Gamby D. Influence of loading rate on transverse ply crack growth in aeronautical CFRP laminates. In: The 11th European conference on composite materials (ECCM 11), Rhodes, Greece; 2004.
7. Experimental and numerical analysis of loading rate and temperature effects on matrix cracking in CFRP laminates
8. Nonlinear viscoelastic micromechanical analysis of fibre-reinforced polymer laminates with damage evolution10.1016/j.ijsolstr.2004.06.021 ↗
9. Three-dimensional, nonlinear viscoelastic analysis of laminated composites10.1177/002199839402801002 ↗
10. Nonlinear viscoelastic and viscoplastic constitutive equations based on thermodynamics10.1023/A:1009767812821 ↗
11. On the characterization by Schapery’s model of non-linear viscoelastic materials10.1016/0142-9418(87)90007-9 ↗
12. Damage mechanics for composite laminates under complex loading
13. Correspondence principle and a generalized J integral for large deformation and fracture analysis of viscoelastic media10.1007/BF01140837 ↗
14. Press · 1992
15. Nguyen TH. Etude expérimentale et modélisation de la cinétique d’endommagement par multifissuration matricielle dans des stratifiés carbone/époxyde soumis à des chargements monotones à vitesse imposée ou à des chargements de fatigue à fréquence imposée (“Experimental study and modelling of damage kinetics induced by matrix transverse cracking in carbon/epoxy laminates subjected to monotonic loading or fatigue loading). PhD thesis, Université de Poitiers, Poitiers, France; 2005.
16. Probabilistic energy based model for prediction of transverse cracking in cross-ply laminates10.1016/j.ijsolstr.2004.06.043 ↗
17. A simplified analysis of transverse ply cracking in cross-ply laminates10.1016/0266-3538(88)90008-5 ↗
18. Ogin SL, Smith PA, Beaumont PWR. Transverse ply crack growth and associated stiffness reduction during the fatigue of a simple crossply laminate. CUED/C/MATS/TR.105, Engineering Department, Cambridge University, UK; 1984.
19. Doubly periodic matrix cracking in composite laminates. Part 1: General in-plane loading10.1016/S0263-8223(96)00071-2 ↗
20. Crack velocity dependent toughness in rate dependent materials10.1016/S0167-6636(00)00031-4 ↗
21. Cracks and crazes: on calculating the macroscopic fracture energy of glassy polymers from molecular simulations10.1103/PhysRevLett.89.148304 ↗
22. Time-dependent crack behavior in an integrated structure10.1023/B:FRAC.0000022238.52635.88 ↗
23. Thin film cracking modulated by underlayer creep10.1007/BF02410525 ↗
24. Formation and growth of 90° ply fatigue cracks in carbon/epoxy laminates10.1016/0266-3538(91)90087-6 ↗
25. Stress–strain behaviour of IM7/977-2 and IM7/APC2 carbon fibre composites at low and high strain rates10.1051/jp4:20020670 ↗
26. The prediction of the long-term mechanical behaviour of aeronautical laminates10.1016/S0266-3538(00)00108-1 ↗
27. Schapery RA. Further development of a thermodynamic constitutive theory: stress formulation, Purdue Research Foundation, Research project number 4958; 1969.