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

Table 7

Performance of five rotors with different forward sweeps of the blade tip.

	(kg/s)			SM (%)
3D-opt rotor	6.37	2.80	0.910	1.59
Tip-forward+0.1	6.37	2.80	0.905	2.34
Tip-forward+0.2	6.38	2.80	0.903	2.72
Tip-forward+0.3	6.38	2.80	0.900	12.52
Tip-forward+0.4	6.39	2.80	0.898	13.86