Research Article
Detailed Parametric Investigation and Optimization of a Composite Wing with High Aspect Ratio
Table 9
Structural performance of different materials.
| | Maximum stress (MPa) | Maximum deformation (mm) | Mass (kg) |
| Full-composite wing | 309.34 | 315 | 220.09 | Full-metal wing | 263.88 | 570.97 | 382.41 | Variation | 17.2% | 44.83% | 42.45% |
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