Open Access
Table 6.
Results of five simulations in different configurations.
| Parameter | Config. A | Config. B | Config. C | Config. D | Config. E |
|---|---|---|---|---|---|
| Material | Epoxy R | Epoxy R | Epoxy R | ABS | ABS |
| Max. Von Mises (N/m2) | 1.987E+8 | 1.243E+8 | 1.303E+8 | 1.987E+8 | 1.243E+8 |
| Max. displacement (mm) | 11.867 | 5.326 | 5.543 | 17.800 | 7.989 |
| Volume (Measure) (m3) | 8.682E−6 | 1.980E−5 | 1.82E−05 | 8.289E−6 | 1.982E−5 |
| Total weight (Drone Structure) (g) | 40.98 | 93.46 | 85.90 | 33.49 | 79.99 |
| Total cost (€) | 12.29 | 28.04 | 25.77 | 0.12 | 0.28 |
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