The Effect of Yaw Angle on a Compressible Rectangular Cavity Flow

Figure 5

The pressure coefficients near the rear corner (x/L = 0.919 and 1.058): (a) M = 0.64, (b) M = 0.70, and (c) M = 0.83.

(a) M = 0.64

(b) M = 0.70

(c) M = 0.83