An investigation of non-linear elastic behavior of CFRP laminates and strain measurement using Lamb waves
Source abstract
Abstract
Abstract This paper investigates the non-linear elastic behavior of unidirectional and cross-ply CFRP laminates and proposes a new method to measure tensile strain using Lamb waves. Young’s modulus was measured as a function of strain in situ using Lamb wave velocity during a tensile test. The stiffening effect of the carbon fibers on [0]8 specimens and the softening effect of the epoxy matrix on [90]8 specimens were accurately evaluated. Young’s modulus of the 0° ply was obtained as a quadratic function of strain. Using the function and the rule of mixture, the dependence of Young’s modulus on strain was accurately predicted for cross-ply laminates. Based on the results, the tensile strain was quantitatively correlated with the corresponding arrival time of the Lamb waves. The strains obtained from the proposed method agreed well with those from the strain gauge. Finally, the effect of transverse cracks on the in situ Young’s modulus of the cross-ply laminate under a tensile load was investigated. This method clearly detected even a small decrease in the Young’s modulus due to the transverse cracks in stiffening cross-ply laminate.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Ultrasonics and Acoustic Wave Propagation · Structural Health Monitoring Techniques · Mechanical Behavior of Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (18)
Show source-provided references
1. Non-hookean behavior of strong carbon fibres10.1038/2201024a0 ↗
2. Strength and modulus of current carbon-fibres10.1016/0008-6223(86)90144-2 ↗
3. Non-hookean stress–strain response and changes in crystallite orientation of carbon fibres10.1007/BF00366347 ↗
4. Non hookean behavior in the fibre direction of carbon-fibre composites and the influence of fibre waviness on the tensile properties10.1177/002199837701100408 ↗
5. Hardening non-linear behavior in longitudinal tension of unidirectional carbon composites10.1007/BF00552401 ↗
6. Variation of elastic moduli with strain in carbon/epoxy laminates10.1177/002199839002401103 ↗
7. Nonlinear stress–strain behavior of graphite/epoxy laminates10.2514/3.9127 ↗
8. Lamb waves in an anisotropic plate. II: Nondestructive evaluation Leaky of matrix cracks on fiber-reinforced composites10.1121/1.401017 ↗
9. Lamb wave assessment of fatigue and thermal damage in composites10.1121/1.422761 ↗
10. Quantitative damage detection in cross-ply laminates using Lamb wave method10.1016/S0266-3538(03)00163-5 ↗
11. Lamb wave method for quick inspection of impact-induced delamination in composite laminates10.1016/j.compscitech.2003.10.011 ↗
12. Ultrasonic velocity studies of composite and heterogeneous materials
13. Inversion of Leaky Lamb wave data by simplex algorithm10.1121/1.399927 ↗
14. How isotropic are quasi-isotropic laminates10.1016/S1359-835X(02)00180-X ↗
15. Plate mode velocities in graphite/epoxy plates10.1121/1.410265 ↗
16. Time-frequency analysis of the dispersion of Lamb modes10.1121/1.426883 ↗
17. Advanced waveform-based acoustic emission detection of matrix cracking in composites
18. One sensor linear location of acoustic emission events using plate wave theories10.1016/S0921-5093(98)01142-3 ↗