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

Table 8

Aerodynamic performance of five rotors with different tip chord lengths.

	(kg/s)	(kg/s)			SM (%)
Tip-forward +0.30	6.38	5.70	2.80	0.900	12.52
Lengthen+0.05	6.38	5.57	2.80	0.901	15.51
Lengthen+0.10	6.38	5.40	2.80	0.902	18.11
Lengthen+0.15	6.38	5.45	2.80	0.903	17.59
Lengthen+0.20	6.39	5.48	2.80	0.904	17.24