Mach number distribution for subsonic flow over a bump.

Supersonic Flow in Corner or over Wedge

Pressure distribution over the test turbine blade, comparison with

Mach Number & Reynolds Number – Introduction to Aerospace Flight Vehicles

Area rule - Wikipedia

Convergence history for subsonic flows over a bump.

Mach number and static pressure contours of the flow calculated in the

ch10-4

CFD Internal Flow in A Channel With Circular Bump, PDF, Computational Fluid Dynamics

Spanwise distribution of pitch averaged loss coefficient ζ, comparison

Snapshot of the argon bubble (d = 0.5 mm) distribution in the symmetry