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

Figure 11

(a) Front view of the supersonic zone around the curved wing (Case , Mach = 0.90, time = 6.5 s). (b) Rear view of the supersonic zone around the curved wing (Case , Mach = 0.90, time = 6.5 s).

(a)

(b)