A Numerical Scheme Based on an Immersed Boundary Method for Compressible Turbulent Flows with Shocks: Application to Two-Dimensional Flows around Cylinders

Figure 9

Pressure contours (left) and time variation of aerodynamic coefficient (right).

(a) M03-A-0050D

(b) M03-A-0050D

(c) M03-B-0050D

(d) M03-B-0050D

(e) M03-C-0050D

(f) M03-C-0050D