Research Article
Multidisciplinary Integrated Framework for the Optimal Design of a Jet Aircraft Wing
Table 2
Level 1 results summary.
| Geometry Loop |
| Airplane data |
| Weight | 686700 N |
| Geometry variables | Best |
| Dimensions: | | Semispan | 17,5 m | Root chord | 8 m | Reference surface | 81,34 m2 | Taper ratio | 0,16 | Aspect ratio | 15,06 | Angles: | | Sweep angle | 25° | Dihedral angle | 5° | Twist angle | 3° | Air foil data: | | Number of air foil | 4 |
| Air foil 4-digit NACA | Position |
| NACA1412 | 0% span | NACA2412 | 30% span | NACA2412 | 60% span | NACA2410 | 100% span |
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