Detection on matrix induced composite failures
Source abstract
Abstract
Abstract As most composite failures are caused by matrix failures, the detection on the latter is of fundamentally importance. This can be achieved only when the homogenized stresses of the matrix obtained from a micromechanics theory are converted into true values. Based on the true stress concept established by the author, the matrix induced composite failures are predicted in this paper. There are essentially two kinds of matrix failures, i.e., tensile or compressive failures, depending on whether the normal stress of the matrix on its failure surface is positive or negative. It has been found that the two kinds of failures correspond to different failure mechanisms. A matrix tensile failure takes place as though the matrix were without any fiber reinforcement, and a quadratic failure criterion developed from Mohr's law suffices to detect such a failure. On the other hand, a compressive failure surface of the matrix can only occur in parallel to the fiber direction, and a matrix compressive failure is controlled by its shear strength. A slippage failure criterion based on the maximum equivalent true shear stress is developed to assess a matrix compression induced composite failure. The input required has been reduced to minimum. Good correlation between predicted and measured failure envelopes of a number of composite systems confirms the efficiency of the proposed failure criteria.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Composite Material Mechanics · Composite Structure Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (48)
Show source-provided references
1. Predicting failure in composite laminates: the background to the exercise10.1016/S0266-3538(98)00074-8 ↗
2. The background to Part B of the Second World-Wide Failure Exercise: evaluation of theories for predicting failure in polymer composite laminates under three-dimensional states of stress10.1177/0021998312473346 ↗
3. Failure of composite materials
4. Assessment of recent theories for predicting failure of composite laminates10.1115/1.2515639 ↗
5. Review of methodologies for composite material modelling incorporating failure10.1016/j.compstruct.2008.03.007 ↗
6. Assessment of the fundamentals of failure theories for composite materials10.1016/j.compscitech.2014.10.014 ↗
7. Paris · 2001
8. A general theory of strength for anisotropic materials10.1177/002199837100500106 ↗
9. Failure criteria for unidirectional fiber composites10.1115/1.3153664 ↗
10. Failure analysis of FRP laminates by means of physically based phenomenological models10.1016/S0266-3538(96)00140-6 ↗
11. Pinho · 2005
12. Multiscale approach for identification of transverse isotropic carbon fibre properties and prediction of woven elastic properties using ultrasonic identification10.1016/j.compscitech.2018.09.016 ↗
13. Compressive response of hybrid 3D woven textile composites (H3DWTCs): an experimentally validated computational model10.1016/j.jmps.2018.08.018 ↗
14. A multiscale modeling for failure predictions of fiber reinforced composite laminates10.1016/j.compositesb.2019.107166 ↗
15. Predicting strength of fibrous laminates under triaxial loads only upon independently measured constituent properties10.1016/j.ijmecsci.2013.08.010 ↗
16. LM Xin, in situ strengths of matrix in a composite10.1007/s10409-016-0611-1 ↗
17. The determination of the elastic field of an ellipsoidal inclusion and related Problems10.1098/rspa.1957.0133 ↗
18. Stress fields in composites reinforced by coated cylindrically orthotropic fibers10.1016/0167-6636(90)90027-D ↗
19. Prediction of interfacial debonding in fiber-reinforced composite laminates10.1002/pc.24943 ↗
20. Simulation of the mechanical properties of fibrous composites by the bridging micromechanics model10.1016/S1359-835X(00)00142-1 ↗
21. Huang · 2018
22. Theoretical prediction of dynamic composite material properties for hypervelocity impact simulations10.1016/j.ijimpeng.2008.12.012 ↗
23. Comparative review study on elastic properties modeling for unidirectional composite materials
24. On micromechanics approach to stiffness and strength of unidirectional composites10.1177/0731684418811938 ↗
25. Lamina properties, lay-up configurations and loading conditions for a range of fibre-reinforced composite laminates10.1016/S0266-3538(98)00078-5 ↗
26. Stress fields in composites with coated inclusions10.1016/0167-6636(89)90021-5 ↗
27. Failure of fiber-reinforced composite laminates under longitudinal compression10.1177/0021998319839217 ↗
28. Failure analysis of FRP laminates by means of physically based phenomenological models10.1016/S0266-3538(01)00208-1 ↗
29. 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 ↗
30. Aragonés · 2007
31. Mechanical behavior of unidirectional fiber-reinforced polymers under transverse compression: microscopic mechanisms and modeling10.1016/j.compscitech.2007.02.001 ↗
32. Failure criteria for FRP laminates10.1177/0021998305046452 ↗
33. Failure criteria for FRP laminates in plane stress
34. Input data for test cases used in benchmarking triaxial failure theories of composites10.1177/0021998312449886 ↗
35. Mechanical properties and details of composite laminates for the test cases used in the third world-wide failure exercise10.1177/0021998313499477 ↗
36. Progressive failure predictions for rib-stiffened panels based on multicontinuum technology10.1016/j.compstruct.2003.11.013 ↗
37. Prediction of the failure locus of C/PEEK composites under transverse compression and longitudinal shear through computational micromechanics10.1016/j.compscitech.2008.07.011 ↗
38. Prediction of in situ strengths and matrix cracking in composites under transverse tension and in-plane shear10.1016/j.compositesa.2005.04.023 ↗
39. Mechanical properties evaluation of T800 carbon fiber reinforced hybrid composite embedded with silicon carbide microparticles: a micromechanical approach10.1108/MMMS-09-2017-0106 ↗
40. Structural design and analysis of composite aircraft fuselage used to develop AFP technology
41. Biaxial test results for strength and deformation of a range of E-glass and carbon fibre reinforced composite laminates: failure exercise benchmark data10.1016/S0266-3538(02)00093-3 ↗
42. A new yield and failure theory for composite materials under static and dynamic loading10.1016/j.ijsolstr.2017.08.036 ↗
43. Interfiber/interlaminar failure of composites under multi-axial states of stress10.1016/j.compscitech.2008.04.016 ↗
44. Characterization of elastic-plastic behavior of AS4/PEEK thermoplastic composite for temperature variation10.1177/002199839102501003 ↗
45. Failure of carbon/epoxy lamina under combined stress10.1177/002199838702100703 ↗
46. Multiaxial characterization of T800/3900-2 carbon/epoxy composites10.1016/0266-3538(92)90009-R ↗
47. Residual stresses in thermoplastic composites—a study of the literature—Part I: formation of residual stresses10.1016/j.compositesa.2005.12.025 ↗
48. Recommendations for designers and researchers resulting from the world-wide failure exercise10.1016/S0266-3538(03)00228-8 ↗