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

Table 1

Materials database.

			Material DB
Aluminium alloys		E [MPa]		𝜈				𝜌 [kg/m^3]
6060	isot1	69000		0,25				2,42
7075	isot2	72000		0,23				2,51
2024	isot3	73000		0,25				2,64
Composites		E11 [MPa]	E22 [MPa]	𝜈	G12 [MPa]	G23 [MPa]	G13 [MPa]	𝜌 [kg/m^3]
Carbon-epoxy	orto1	92600	7730	0,36	3820	3820	3820	1,1
Graphite-ep. 01	orto2	130000	10000	0,31	4850	3620	3620	1,2
Graphite-ep. 02	orto3	132160	8650	0,3	4120	4120	4120	1,3