Research Article
Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio
Figure 23
Mach number contours at 90% span of the five rotors at the design point.
(a) 3D-opt rotor |
(b) Tip-forward+0.1 |
(c) Tip-forward+0.2 |
(d) Tip-forward+0.3 |
(e) Tip-forward+0.4 |