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 m^2
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