Multidisciplinary Integrated Framework for the Optimal Design of a Jet Aircraft Wing

Table 3

Level 2, mission optimization loop results summary.

Mission optimization
Performance objectives
𝑊fuel	Min
E	Max
Mission condition
mission phase	cruise
Range	5120 nm
Altitude	10000 m
T	223,15 K
a	299,46 m/s
p	2,64E + 04 Pa
rho	0,4127 kg/m^3
Mission variables	Best
Airspeed	279,42 m/s
Alfa	6,88°
CL	0,96
CD	0,04
Re	30346949,63
M	0,93
Optimum objective variables
E	21,97
𝑊fuel	140280 N