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

Table 3

Comparison between performances of the original and optimized profiles.

Span			(deg)
10%	Target	1.13	55.8	2.80	2.05	0.900
	Initial	1.10	59.8	2.78	1.84	0.910
	Optimal	1.14	57.3	2.79	1.94	0.931
50%	Target	1.35	61.6	2.80	2.23	0.900
	Initial	1.30	67.6	2.75	1.86	0.853
	Optimal	1.32	63.0	2.78	1.91	0.904
90%	Target	1.57	66.2	2.80	2.46	0.900
	Initial	1.59	67.5	2.77	2.18	0.884
	Optimal	1.59	66.8	2.80	2.21	0.910