Multiscale progressive damage analysis of CFRP composites using a mechanics based constitutive relation
Source abstract
Abstract
Abstract A continuum damage mechanics-based material model for the constituent phases of a carbon fiber reinforced polymer composite material is presented. This constitutive model is applied to Eigenstrain based Reduced-order Homogenization framework for multiscale modeling. A key contribution is that all model parameters are directly or indirectly calibrated using experimental data and these model parameters can be readily updated by describing the evolution of damage as a function of the strain state. The constitutive model for polymer matrix captures mixed mode from pure uniaxial to pure shear loading without using any conventional failure criterion. The accuracy of the constitutive model is demonstrated by comparing experimental results of unnotched and open-hole laminates. In addition, a demonstration is presented to alleviate spurious residual stiffness appearing from the reduction of model order of the microstructure.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Material Mechanics · Mechanical Behavior of Composites · Numerical methods in engineering
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (38)
Show source-provided references
1. Department of Defense, Composite Materials Handbook, F Edition, vol. 2. Polymer Matrix Composites Materials Properties. SAE International; 2002.
2. NASA. Advanced composites partnership [Tech. rep.]. NASA; 2014.
3. Liu X, Furrer D, Kosters J, Holmes J. Vision 2040: A roadmap for integrated, multiscale modeling and simulation of materials and systems [Technical Report NASA/CR-2018-219771, E-19477, GRC-E-DAA-TN52454]. NASA; 2018.
4. Physically-based failure models and criteria for laminated fibre-reinforced composites with emphasis on fibre kinking: part I: development10.1016/j.compositesa.2005.04.016 ↗
5. Physically based failure models and criteria for laminated fibre-reinforced composites with emphasis on fibre kinking. Part II: FE implementation10.1016/j.compositesa.2005.06.008 ↗
6. Modelling complex progressive failure in notched composite laminates with varying sizes and stacking sequences10.1016/j.compositesa.2013.11.012 ↗
7. Progressive damage analysis as a design tool for composite bonded joints10.1016/j.compositesb.2015.03.046 ↗
8. Progressive damage modeling of open-hole composite laminates under compression10.1016/j.compstruct.2014.12.022 ↗
9. Numerical simulation of progressive damage and failure in composite laminates using XFEM/CZM coupled approach10.1016/j.compositesa.2016.12.026 ↗
10. A blended continuum damage and fracture mechanics method for progressive damage analysis of composite structures using XFEM10.1016/j.compstruct.2017.10.007 ↗
11. A multiscale progressive failure approach for composite laminates based on thermodynamical viscoelastic and damage models10.1016/j.compositesa.2006.01.018 ↗
12. Validated progressive damage analysis of simple polymer matrix composite laminates exhibiting matrix microdamage: comparing macromechanics and micromechanics10.1016/j.compscitech.2016.07.018 ↗
13. A multiscale progressive damage analysis for laminated composite structures using the parametric HFGMC micromechanics10.1016/j.compstruct.2017.11.089 ↗
14. Fish · 2013
15. Eigendeformation-based reduced order homogenization for failure analysis of heterogeneous materials10.1016/j.cma.2006.08.015 ↗
16. Symmetric mesomechanical model for failure analysis of heterogeneous materials10.1615/IntJMultCompEng.v8.i5.20 ↗
17. Experimental and computational investigation of progressive damage accumulation in CFRP composites10.1016/j.compositesb.2012.12.005 ↗
18. Prediction of progressive damage and strength of IM7/977-3 composites using the Eigendeformation-based homogenization approach: static loading10.1177/0021998316650982 ↗
19. Moisture and temperature effects of the compressive failure of cfrp unidirectional laminates10.1177/002199839703100805 ↗
20. Gilat A, Goldberg RK, Roberts GD. Strain rate sensitivity of epoxy resin in tensile and shear loading. J Aerospace Eng.
21. Measurement of epoxy resin tension, compression, and shear stress–strain curves over a wide range of strain rates using small test specimens10.1061/(ASCE)0893-1321(2008)21:3(162) ↗
22. Rate-dependent damage model for polymeric composites under in-plane shear dynamic loading10.1016/j.commatsci.2014.04.067 ↗
23. An investigation of matrix damage in composite laminates using continuum damage mechanics10.1016/j.compstruct.2015.06.012 ↗
24. Modelling the nonlinear shear stress-strain response of glass fibre-reinforced composites. Part I: experimental results10.1016/j.compscitech.2005.04.014 ↗
25. Nonlinear anisotropic elasticity for laminate composites10.1007/s11012-015-0104-5 ↗
26. Modelling the nonlinear shear stress-strain response of glass fibre-reinforced composites. Part II: model development and finite element simulations10.1016/j.compscitech.2005.04.018 ↗
27. Nonlinear shear behavior and failure of composite materials under plane stress conditions10.1007/s00707-017-1817-4 ↗
28. FE2 multiscale approach for modelling the elastoviscoplastic behavior of long fiber SiC/Ti composite materials10.1016/S0045-7825(99)00224-8 ↗
29. On the equivalent inclusion method and impotent eigenstrains10.1007/BF00041098 ↗
30. Hybrid impotent-incompatible eigenstrain base homogenization10.1002/nme.4473 ↗
31. The method of failure paths for reduced-order computational homogenization10.1615/IntJMultCompEng.2016018702 ↗
32. ASTM Standard 3039 · 2008
33. ASTM Standard D3410 · 2008
34. Experimental results of quasi-static testing for calibration and validation of composite progressive damage analysis methods10.1177/0021998316658539 ↗
35. Cytec Engineered Materials. CYCOM 977-3 epoxy resin system technical data sheet; 2012. URL:https://www.cytec.com/sites/default/files/datasheets/CYCOM_977_3.pdf.
36. Pinho ST, Davila CG, Camanho PP, Iannucci L, Robinson P. Failure models and criteria for FRP under in-plane or three-dimensional stress states including shear non-linearity, techreport WU 23-064-30-22. NASA; 2005. URL:https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20050110223.pdf.
37. Three-dimensional invariant-based failure criteria for fibre-reinforced composites10.1016/j.ijsolstr.2014.03.038 ↗
38. Comparison of composite damage growth tools for static behavior of notched composite laminates10.1177/0021998316675945 ↗