Abstract
In present study, laminates with the type of [±θ°]S and [0°2/±θ°]S are investigated in order to clearly show the effect of material shear nonlinearity, and then theoretical predictions are compared with experimental data. In the whole process of generating failure envelopes, secant shear modulus instead of initial shear modulus is used for accurate shear stress-strain relation. The modulus values are recalculated every time when the combining load is changed. Final failure envelopes are then compared between numerical models. It is found that the variation in the size of safe regions from nonlinear analysis is closely related to the way of combing load and fiber directions. So in the process of improving failure theories or in the applications of failure theories, the effect of material nonlinearity can be considered appropriately.
Similar content being viewed by others
Abbreviations
- FF, MF, SF :
-
Fiber failure, matrix failure, shear failure
- XT, XC :
-
Longitudinal tensile strength, compressive strength
- YT, YC :
-
Transverse tensile strength, compressive strength
- S :
-
In-plane shear strength
- L, NL :
-
Linear analysis, nonlinear analysis
- R ⊥⊥ A :
-
Fracture resistance against the fracture
- p⊥⊥(+),p⊥⊥− :
-
Inclination parameters of (σn, τnt)σn=0 fracture curves
- p⊥‖(+), p⊥‖(-) :
-
Inclination parameters of (σn, τnl)σn=0 fracture curves
- ηr:
-
Residual stiffness
- c, ξ:
-
Fitting experimental data parameters
References
J. D. Schaefer and I. M. Daniel, Strain-rate-dependent yield criteria for progressive failure analysis of composite laminates based on the northwestern failure theory, Experimental Mechanics, 58 (3) (2018) 1–11.
B. Werner, J. Schaefer and I. Daniel, Deformation and failure of angle-ply composite laminates, Experimental Mechanics of Composite, Hybrid, and Multifunctional Materials, Proceedings of the 2013 Annual Conference on Experimental and Applied Mechanics, Springer International Publishing Company, USA (2014) 167–171.
G. Seon, A. Makeev, J. D. Schaefer and B. P. Justusson, DIC data driven methods to verify simplifying assumptions and increase confidence in material properties of laminated composites, American Society of Composites 32nd Technical Conference (2017).
C. T. Sun, J. Tao and A. S. Kaddour, The prediction of failure envelopes and stress/strain behaviour of composite laminates: Comparison with experimental results, Composites Science and Technology, 62 (12–13. (2002) 1673–1682.
T. A. Bogetti et al., Predicting the nonlinear response and failure of composite laminates: Correlation with experimental results, Composites Science and Technology, 64 (3) (2004) 477–485.
T. S. Butalia and W. E. Wolfe, Strain energy based non-linear failure criterion: Comparison of numerical predictions and experimental observations for symmetric composite laminates, Composite Science and Technology, 62 (12–13. (2002) 1697–1710.
B. Zand, T. S. Butalia, W. E. Wolfe and G. A. Schoeppner, A strain energy based failure criterion for nonlinear analysis of composite laminates subjected to triaxial loading, Journal of Composite Materials, 46 (19–20). (2012) 2515–2537.
B. M. Doudican et al., Strain energy based failure criterion: comparison of numerical predictions and experimental observations for symmetric composite laminates subjected to triaxial loading, Journal of Composite Materials, 47 (6–7. (2012) 847–866.
T. A. Bogetti et al., Predicting the nonlinear response and progressive failure of composite laminates under triaxial loading: Correlation with experimental results, Journal of Composite Materials, 47 (6–7). (2013) 793–804.
A. S. Kaddour, M. J. Hinton and P. D. Soden, A comparison of the predictive capabilities of current failure theories for composite laminates: Additional contributions, Composites Science and Technology, 64 (3–4. (2004) 449–476.
A. S. Kaddour and M. J. Hinton, Benchmarking of triaxial failure criteria for composite laminates: Comparison between models of ‘Part (A)’ of ‘WWFE-II’, Journal of Composite Materials, 46 (19–20. (2012) 2595–2634.
A. S. Kaddour, M. J. Hinton, P. A. Smith and S. Li, A comparison between the predictive capability of matrix cracking, damage and failure criteria for fibre reinforced composite laminates: Part A of the third world-wide failure exercise, Journal of Composite Materials, 47 (20–21. (2013) 2749–2779.
P. P. Camanho et al., Three-dimensional invariant-based failure criteria for fibre reinforced composites, International Journal of Solids and Structures, 55 (2015) 92–107.
A. Puck and H. Schürmann, Failure analysis of FRP laminates by means of physically based phenomenological models, Composite Science and Technology, 58 (7)(1998) 1045–1068.
A. Puck, J. Kopp and M. Knops, Guidelines for the determination of the parameters in Puck’s action plane strength criterion, Composite Science and Technology, 62 (3)(2002) 371–378.
NASA Langley Research Center, Failure Models and Criteria for FRP Under In-Plane or Three-Dimensional Stress States Including Shear Non-Linearity, USA (2005).
W. P. Lin and H. T. Hu, Nonlinear analysis of fiber-reinforced composite laminates subjected to uniaxial tensile load, J. of Composite Materials, 36 (12)(2002) 1429–1450.
F. Hassani, M. M. Shokrieh and L. B. Lessard, A fully nonlinear 3D constitutive relationship for the stress analysis of a pin-loaded composite laminate, Composite Science and Technology, 62 (3)(2002) 429–439.
C. T. Sun and J. L. Chen, A micromechanical model for plastic behavior of fibrous composites, Composite Science and Technology, 40 (2)(1991) 115–129.
R. Haj-Ali and H. Kilic, Nonlinear constitutive models for pultruded FRP composites, Mechanics of Materials, 35 (8)(2003) 791–801.
F. A. Leone, Deformation gradient tensor decomposition for representing matrix cracks in fiber-reinforced composite structures, Composites Part A, 76 (2015) 334–341.
J. D. Schaefer, B. T. Werner and I. M. Daniel, Strain-rate-dependent failure of a toughened matrix composite, Experimental Mechanics, 54 (6)(2014) 1111–1120.
P. P. Theodore and E. A. Alexandros, A progressive damage FEA model for glass/epoxy shell structures, Journal of Composite Materials, 47 (5)(2013) 623–637.
M. Knops, Sukzessives Bruchgeschehen in Faserverbundlaminaten, Ph.D Thesis, RWTH, Verlag Mainz, Aachen (2003).
P. D. Soden, M. J. Hinton and A. S. Kaddour, Lamina properties, lay-up configurations and loading conditions for a range of fibre-reinforced composite laminates, Composite Science and Technology, 58 (7)(1998) 1011–1022.
H. L. Jia, H. I. Yang and T. W. Kang, The influence of material shear nonlinearity on multidirectional laminates in terms of failure envelopes, Journal of Mechanical Science and Technology, 32 (12)(2018) 5823–5829.
Author information
Authors and Affiliations
Corresponding author
Additional information
Recommended by Editor Seungjae Min
Hyun-Ik Yang, Ph.D., is a Professor in the Dept. of Mechanical Engineering of College of Engineering Science ERICA Hanyang University. He received Ph.D. in Mechanical Engineering from Columbia University in the City of New York. His research interests include mechanical system design, CAD/mesh generation and hydrogen generation.
Rights and permissions
About this article
Cite this article
Jia, H., Yang, HI., Kim, C.W. et al. The influence of material shear nonlinearity on predictive failure envelopes of multidirectional laminates. J Mech Sci Technol 34, 1645–1653 (2020). https://doi.org/10.1007/s12206-020-0327-9
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s12206-020-0327-9