Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio

Figure 15

Mach number contours of 90% span at the design point.

(a) 3D-opt rotor

(b) Shroud+1 mm

(c) Shroud+2 mm

(d) Shroud+3 mm

(e) Shroud+4 mm