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

Table 6

Aerodynamic performance of five rotors.

	(kg/s)			SM (%)
3D-opt rotor	6.37	2.80	0.910	1.59
Shroud+1 mm	6.37	2.80	0.901	3.52
Shroud+2 mm	6.38	2.80	0.895	4.77
Shroud+3 mm	6.38	2.80	0.888	5.78
Shroud+4 mm	6.38	2.80	0.880	8.95