Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors

Table 3

Performance of the two rotors at 70% design speed.

Blade	δ (mm)	(kg/s)				(%)
Rotor37	0.25	15.889	1.377	0.9173	/	0.51
	0.50	15.998	1.365	0.9171	-0.02%	0.99
	0.75	15.994	1.363	0.9157	-0.14%	1.50
	1.00	15.904	1.359	0.9142	-0.29%	2.03
RotorSD	0.25	14.651	1.318	0.8884	/	0.49
	0.50	14.605	1.317	0.8883	-0.01%	1.03
	0.75	14.593	1.314	0.8881	-0.02%	1.63
	1.00	14.567	1.311	0.8877	-0.06%	2.27