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

Table 2

CFD boundary conditions.

	Swept wing model	Curved wing model
Altitudes analysed	0 m–10000 m	0 m–10000 m
Pressure far field	Front side up down	Front side up down
Pressure outlet	Rear	Rear
Symmetry	Center-line plane	Center-line plane
Wall/no slip	Wing surface	Wing surface