Elementary Liber Fibres Characterisation: Bias from the Noncylindricity and Morphological Evolution along the Fibre
Abstract
:1. Introduction
2. Materials and Methods
2.1. Material—Measured Fibres
2.2. Sample Preparation for Optical Microscope Cross-Section Observation
2.3. Optical Microscope—Axial Observations of Fibre Cross Sections
2.4. Optical Microscope—Transverse Uni and Bi-Directional Cross-Section Measurement
2.5. Dia-Stron Ltd FDAS—Multi-Directional Cross-Section Measurement
2.6. Measurement of Twist
2.7. Elementary Fibre Tensile Test Using LEX820 Device
2.8. Isogeometric Numerical Model of the Fibre
2.9. Identification of the Modulus from Simulation and Analytically
- In terms of stress at failure, the concept of an average section is not necessarily the most appropriate, considering the fact that, at failure, the smallest section exhibits a higher stress than a mean section. This is illustrated in Figure 6, where the colour represents the level of von Mises stress, which is obviously not constant along a fibre since the section area evolves.Assuming again that the material exhibit a similar behaviour at failure along the fibre, the failure is likely to occur in the smallest section, where the stresses are maximal. For evaluating the stress at failure, we recommend using the smallest section along the fibre instead of a mean section.
- In terms of the elastic modulus, considering the assumption of a mean section in Dia-Stron software, an elastic modulus is identified based on Formula (1):The total stiffness of a fibre is the combination of all the local stiffness along the fibre (such as springs put in series) since the total elongation is the sum of all the local elongations. The numerical model proposed in Section 2.8 with varying sections (Figure 6) naturally takes this aspect into account. From a practical point of view, the fibre modulus is identified by the inverse approach, taking an experimental extension of the fibre and adjusting the elastic modulus on the model in order to obtain a resulting tension in the fibre corresponding to the load measured experimentally.Alternatively, if we neglect the geometric nonlinearity and consider a constant stress within a given section, as soon as the evolution of the section is known along the fibre, a similar identification can be performed considering the 1D integral (Equation (4)). This equation is obtained assuming that the total elongation of the fibre comes from the local strains, which are considered depending on the local section of the fibre (Equation (2)) (constant stress within the section):In a discreet manner, considering a number of sections equally distributed of along the fibre (similar to what we face on the scanning device with a discrete number of slices), Equation (4) can be rewritten as Equation (6), introducing the average section and average of the inverse of the sections and considering the fact that :
2.10. Statistical Analysis
3. Results
3.1. Influence of the Chosen Calculation Method on the Section Area of an Individual Fibre and Comparison with the Real Section
3.2. The Impact of the Use of Optical Microscopy on the Cross-Sectional Measurements of Individual Fibres
3.3. Measurement of Apparent Widths by the FDAS System
3.4. Fibre Section Area and Circularity Evolution along Their Lengths
3.5. Natural Twist
3.6. Elastic Modulus and Stress at Failure
- , defined in Section 2.8, represents the gain in terms of identified elastic modulus between the average elliptical section and the model with varying section.
- represents the ratio between the average section and the minimal section, which is also the expected gain in terms of stress at failure.
4. Discussion
- Circularity is not high enough;
- The cross-sectional area varies greatly along the fibre.
5. Conclusions
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
References
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Real Measured Area (µm²) | Difference (%)/Measured Area ImageJ | ||||
---|---|---|---|---|---|
Elliptical Model | Circular Model (Large Diameter) | Circular Model (Small Diameter) | Circular Model (Mean Diameter) | ||
Mean | 163 | +2 | +129 | −48 | +21 |
Standard-deviation | 110 | 5 | 120 | 16 | 26 |
Average Section Elliptical Model (µm²) | Difference (%)/Elliptical Model | ||
---|---|---|---|
Average Section Circular Model FDAS | Average Section Circular Model Microscopy | ||
Linseed flax | 150.6 | +31 | +55 |
Textile flax | 73.8 | +16 | +46 |
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Grégoire, M.; De Luycker, E.; Ouagne, P. Elementary Liber Fibres Characterisation: Bias from the Noncylindricity and Morphological Evolution along the Fibre. Fibers 2023, 11, 45. https://doi.org/10.3390/fib11050045
Grégoire M, De Luycker E, Ouagne P. Elementary Liber Fibres Characterisation: Bias from the Noncylindricity and Morphological Evolution along the Fibre. Fibers. 2023; 11(5):45. https://doi.org/10.3390/fib11050045
Chicago/Turabian StyleGrégoire, Marie, Emmanuel De Luycker, and Pierre Ouagne. 2023. "Elementary Liber Fibres Characterisation: Bias from the Noncylindricity and Morphological Evolution along the Fibre" Fibers 11, no. 5: 45. https://doi.org/10.3390/fib11050045
APA StyleGrégoire, M., De Luycker, E., & Ouagne, P. (2023). Elementary Liber Fibres Characterisation: Bias from the Noncylindricity and Morphological Evolution along the Fibre. Fibers, 11(5), 45. https://doi.org/10.3390/fib11050045