Influence of Upstream and Downstream Compressor Stators on Rotor Exit Flow Field

Table 1

The Purdue 3-Stage Compressor design airfoil parameters.

	IGV	R1	S1	R2	S2	R3	S3
# of blades	44	36	44	33	44	30	50
Solidity	1.27	1.37	1.34	1.33	1.42	1.28	1.70
AR	1.00	0.76	0.95	0.72	0.90	0.68	0.85
Mach; number	0.26; (abs)	0.46; (rel)	0.35; (abs)	0.45; (rel)	0.33; (abs)	0.44; (rel)	0.31; (abs)