Aeroelastic Analysis of Wings in the Transonic Regime: Planform’s Influence on the Dynamic Instability

Table 1

Geometrical data of the two half-wing models.

	Swept wing	Curved wing
AR (aspect ratio)	9.5	9.5
Angle of sweep at root	32°	32°
Angle of sweep at tip	32°	53°
Half-wing span (/2)	30 m	30 m
Reference surface area	379 m^2	379 m^2
Root chord	13.18 m	13.18 m
Tip chord	1.7 m	1.7 m
Kink section position (/2)	9.3 m	9.3 m
Kink chord	7.373 m	7.373 m
Dihedral angle	5°	5°