Submitted:
23 September 2024
Posted:
24 September 2024
You are already at the latest version
Abstract
Keywords:
1. Introduction
2. Materials and Methods
| Author | Methodology | Properties | Material | ANOVA | Parameters |
|---|---|---|---|---|---|
| [31] | Numerical | Warpage deformation | PEI ABS PA 6 |
81 samples | PT, PS, BT, ID, LT, IP |
| [32] | Experimental | Flexural strength | ABS | 25 samples | ID 15-100 RA 0-90 NT 20-60 LT 0.1-0.3 BT 90-110 |
| [33] | Experimental | Tensile strength Maximum load Elongation Elastic modulus |
Wood-PLA | 9 samples | LT 0.1-0.3 ID 50-100 PS 10-20 NT 180-190 |
| [34] | Numerical | Residual stress | ABS | 27 samples | PO H,S,V RA 0 -90 IP 0,Z,90 |
| [35] | Experimental | Compressive strength | TPU PLA |
9 samples | PS 40-60 LT 0.1-0.3 ID 50 75 100 |
| Current work | Experimental | Toughness Max. Tensile Strength Elastic Modulus Load @ Max Tensile Strength. |
PLA | 27 samples | PS 60-80 LT 0.1-0.3 ID 15 17.5 20 |
3. Results
3.1. Experimental and Analysis of the Mechanical Properties
3.2. Influence of Infill Density on the Material Properties
3.3. Influence of Layer Thickness on the Properties of the Printed Samples
3.4. ANOVA Results and Discussions
3.5. Regression Analysis and Look-Up Chart
4. Conclusions
Author Contributions
Competing interest
References
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| Infill Density | Print Speed (mm/s) | Layer Thickness (mm) | Maximum Tensile Stress (Mpa) |
Load at Maximum Tensile Stress (kN) | Modulus Of Elasticity (Mpa) | |
|---|---|---|---|---|---|---|
| A | 15 | 60 | 0.1 | 24.143 | 844.99 | 907.05 |
| B | 15 | 60 | 0.2 | 24.39 | 853.64 | 869.85 |
| C | 15 | 60 | 0.3 | 24.271 | 849.5 | 755.16 |
| D | 15 | 70 | 0.1 | 34.276 | 1199.6 | 400.28 |
| E | 15 | 70 | 0.2 | 23.886 | 836 | 889.46 |
| F | 15 | 70 | 0.3 | 23.799 | 832.95 | 840.2 |
| G | 15 | 80 | 0.1 | 22.126 | 774.4 | 864.57 |
| H | 15 | 80 | 0.2 | 22.964 | 803.73 | 736.16 |
| I | 15 | 80 | 0.3 | 23.371 | 818 | 783.03 |
| J | 17.5 | 60 | 0.1 | 25.737 | 900.78 | 930.27 |
| K | 17.5 | 60 | 0.2 | 23.924 | 837.33 | 856.84 |
| L | 17.5 | 60 | 0.3 | 22.888 | 801.08 | 912.13 |
| M | 17.5 | 70 | 0.1 | 23.765 | 831.78 | 824.83 |
| N | 17.5 | 70 | 0.2 | 18.044 | 631.53 | 667.78 |
| O | 17.5 | 70 | 0.3 | 21.465 | 751.28 | 824.81 |
| P | 17.5 | 80 | 0.1 | 24.391 | 853.7 | 887.36 |
| Q | 17.5 | 80 | 0.2 | 22.344 | 782.06 | 840.45 |
| R | 17.5 | 80 | 0.3 | 22.244 | 778.55 | 884.38 |
| S | 20 | 60 | 0.1 | 20.822 | 728.78 | 846.7 |
| T | 20 | 60 | 0.2 | 22.803 | 798.1 | 865.79 |
| U | 20 | 60 | 0.3 | 23.181 | 811.33 | 774.8 |
| V | 20 | 70 | 0.1 | 21.382 | 748.36 | 777.83 |
| W | 20 | 70 | 0.2 | 23.13 | 809.54 | 796.75 |
| X | 20 | 70 | 0.3 | 22.951 | 803.3 | 852.02 |
| Y | 20 | 80 | 0.1 | 22.573 | 790.04 | 812.27 |
| Z | 20 | 80 | 0.2 | 22.908 | 801.79 | 849.08 |
| A1 | 20 | 80 | 0.3 |
| Standard deviation | ||||
| Infill density | Modulus | Max load | Max tensile | Comment |
| 20 | 33.67709 | 28.71557 | 0.820477 | Lowest |
| 17.5 | 72.60368 | 72.16459 | 2.061845 | Medium |
| 15 | 146.6796 | 119.5735 | 3.416865 | Large |
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