Figures & data
Figure 1. An overview of the rectilinear infill designs (60 mm × 10 mm × 10 mm): top view of the infill structure, infill spacing, infill angles, and their corresponding extrusion length.
![Figure 1. An overview of the rectilinear infill designs (60 mm × 10 mm × 10 mm): top view of the infill structure, infill spacing, infill angles, and their corresponding extrusion length.](/cms/asset/a8940c20-2e30-4dff-97a4-5a8185062546/nvpp_a_2349679_f0001_oc.jpg)
Figure 2. A: simulated stress over flexure strain of the designs varied in infill angles. B: relative flexure modulus calculated based on A. C: measured flexure stress over flexure strain (0 to 0.07) based on three-point bending tests (n = 2). D: flexure modulus (Pa) calculated based on the stress-strain curves shown in C, the error bar represents standard deviation from duplicated measurements. Significant differences (P < 0.05) are indicated by the lowercase letters.
![Figure 2. A: simulated stress over flexure strain of the designs varied in infill angles. B: relative flexure modulus calculated based on A. C: measured flexure stress over flexure strain (0 to 0.07) based on three-point bending tests (n = 2). D: flexure modulus (Pa) calculated based on the stress-strain curves shown in C, the error bar represents standard deviation from duplicated measurements. Significant differences (P < 0.05) are indicated by the lowercase letters.](/cms/asset/5bdeec9d-74a6-4175-b17e-355e40d8daa1/nvpp_a_2349679_f0002_oc.jpg)
Figure 3. Measured flexure stress over flexure strain of the designs varied in infill angles obtained from three-point bending tests (n = 2).
![Figure 3. Measured flexure stress over flexure strain of the designs varied in infill angles obtained from three-point bending tests (n = 2).](/cms/asset/b6983ecf-f016-459d-aced-17974e42a418/nvpp_a_2349679_f0003_oc.jpg)
Figure 4. A: texture map (fracture strain vs fracture stress) of 3D-printed samples varied in infill angles. B: DIC strain map of a 3D-printed sample with 30° infill angle at fracture point. C: DIC strain map of a 3D-printed sample with 90° infill angle at fracture point. D: texture map (failure strain vs fracture stress) of 3D-printed samples varied in infill angles. E: DIC strain map of a 3D-printed sample with 30° infill angle at failure point. F: DIC strain map of a 3D-printed sample with 90° infill angle at failure point. The heatmap represents the strain changes with respect to the undeformed image of each sample.
![Figure 4. A: texture map (fracture strain vs fracture stress) of 3D-printed samples varied in infill angles. B: DIC strain map of a 3D-printed sample with 30° infill angle at fracture point. C: DIC strain map of a 3D-printed sample with 90° infill angle at fracture point. D: texture map (failure strain vs fracture stress) of 3D-printed samples varied in infill angles. E: DIC strain map of a 3D-printed sample with 30° infill angle at failure point. F: DIC strain map of a 3D-printed sample with 90° infill angle at failure point. The heatmap represents the strain changes with respect to the undeformed image of each sample.](/cms/asset/28f9e0a5-b5aa-404a-ba81-16385c12b8f8/nvpp_a_2349679_f0004_oc.jpg)
Figure 5. A: simulated stress over flexure distance of the designs varied in infill angle orientations (Bi: binary alternation, Tri: ternary alternation). B: relative flexure modulus calculated based on A. C: measured flexure stress over flexure strain (0 to 0.07) based on three-point bending tests. D: flexure modulus (Pa) calculated based on B. The error bar represents the standard deviation from duplicate measurements. No significant differences (P > 0.05) are found.
![Figure 5. A: simulated stress over flexure distance of the designs varied in infill angle orientations (Bi: binary alternation, Tri: ternary alternation). B: relative flexure modulus calculated based on A. C: measured flexure stress over flexure strain (0 to 0.07) based on three-point bending tests. D: flexure modulus (Pa) calculated based on B. The error bar represents the standard deviation from duplicate measurements. No significant differences (P > 0.05) are found.](/cms/asset/d93ea149-9d03-4130-b2b6-42e0ddf369a4/nvpp_a_2349679_f0005_oc.jpg)
Figure 6. Measured flexure stress over flexure strain of the designs varied in infill angle orientations obtained from three-point bending tests (n = 2).
![Figure 6. Measured flexure stress over flexure strain of the designs varied in infill angle orientations obtained from three-point bending tests (n = 2).](/cms/asset/f5852119-acf2-4662-8115-2e790e1c5e7e/nvpp_a_2349679_f0006_oc.jpg)
Figure 7. A: texture map (fracture strain vs fracture stress) of 3D-printed samples varied in infill angle orientations (Bi: binary alternation, Tri: ternary alternation). B: texture map (failure strain vs fracture stress) of 3D-printed samples varied in infill angle orientations. C: DIC strain maps of 3D-printed samples varied in infill angle orientations at failure point. The right circles indicate the failure positions on each sample.
![Figure 7. A: texture map (fracture strain vs fracture stress) of 3D-printed samples varied in infill angle orientations (Bi: binary alternation, Tri: ternary alternation). B: texture map (failure strain vs fracture stress) of 3D-printed samples varied in infill angle orientations. C: DIC strain maps of 3D-printed samples varied in infill angle orientations at failure point. The right circles indicate the failure positions on each sample.](/cms/asset/81ad0db7-fc29-4a72-8491-7420cc96ebe3/nvpp_a_2349679_f0007_oc.jpg)
Figure 8. Frontal (top) and transversal (bottom) X-ray scans of no-alternation at 30° infill angle (A), binary alternation at 30° infill angle (B), ternary alternation at 30° infill angle (C), no-alternation at 75° infill angle (D), binary alternation at 75° infill angle (E), ternary alternation at 75° infill angle (F). The red arrows indicate the cavities and improper overhangs.
![Figure 8. Frontal (top) and transversal (bottom) X-ray scans of no-alternation at 30° infill angle (A), binary alternation at 30° infill angle (B), ternary alternation at 30° infill angle (C), no-alternation at 75° infill angle (D), binary alternation at 75° infill angle (E), ternary alternation at 75° infill angle (F). The red arrows indicate the cavities and improper overhangs.](/cms/asset/88b628bb-553f-43eb-a850-e2f46436e4c2/nvpp_a_2349679_f0008_oc.jpg)
Figure 9. A: original (top) and modified (bottom) 75° infill design. B: measured flexure stress over flexure strain of original (75) and modified (75 m) infill structures. C: texture map (fracture strain vs fracture stress) of original (75) and modified (75 m) infill structures. D: texture map (failure strain vs fracture stress) of original (75) and modified (75 m) infill structures.
![Figure 9. A: original (top) and modified (bottom) 75° infill design. B: measured flexure stress over flexure strain of original (75) and modified (75 m) infill structures. C: texture map (fracture strain vs fracture stress) of original (75) and modified (75 m) infill structures. D: texture map (failure strain vs fracture stress) of original (75) and modified (75 m) infill structures.](/cms/asset/84270ee5-67bb-4d3e-91de-c07fba95a6f7/nvpp_a_2349679_f0009_oc.jpg)
Data availability statement
The data obtained from this study are available from the corresponding author, LZ, upon reasonable request.