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

Figure 12

(a) Front view of the supersonic zone around the swept wing (Case , Mach = 0.875, time = 7 s). (b) Rear view of the supersonic zone around the swept wing (Case , Mach = 0.875, time = 7 s).

(a)

(b)