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International Journal of Bioprinting                 3D printing of continuous fiber reinforced PLA/PGA composites


























            Figure 5. (A) Thermogravimetric analysis (TGA) and (B) differential scanning calorimetry (DSC) curves of polyglycolic acid (PGA) and polylactic
            acid (PLA).



























            Figure 6. (A) Stress–strain curves of specimens with different layer thicknesses and (B) tensile strengths of specimens with different layer thicknesses.
            The tests were used to determine significant differences between groups (****p < 0.0001; “•” represents the tensile test results of each specimen).


            respectively. The heat flow curve in Figure 5B shows that   were very similar, so the average value was used to plot the
            the  melting points of the PLA and PGA materials were   stress-strain curves. Figure 6 shows the effect of the layer
            152.7°C and 212.0°C, respectively. From the thermal   thickness on the tensile strength. Significant differences
            analysis results, the temperature range for PLA material   were found between the three printing layer thickness
            printing was 152.7°C–347.7°C, and to avoid the PGA   (p < 0.0001), as the layer thickness increased from 0.15 mm
            material melting, the printing temperature should be kept   (scheme 1) to 0.25 mm (scheme 3), the composite specimen
            below 212°C. Therefore, the printing temperature was set   tensile strength decreased from 127.67 ± 2.31 MPa to
            to 210°C in this study.                            61.72 ± 2.58 MPa, decreasing by 106.9%. Figure 7 shows
                                                               the effect of the printing spacing on the tensile strength.
            3.2. Results of tensile tests                      The specimens with 0.25-mm printing spacing exhibited
            The stress–strain curves and tensile strength results for   a significant difference in tensile strength compared to the
            the effect of layer thickness on mechanical properties are   other two printing spacings. By increasing the printing
            summarized in Figures 6–8 and Table 2. The stress–strain   space from 0.25 mm (scheme 4) to 0.40 mm (scheme 5),
            curves of each specimen with the same process parameters   the tensile strength decreased from 209.32 ± 8.37 MPa to


            Volume 9 Issue 4 (2023)                        277                         https://doi.org/10.18063/ijb.734
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