A Novel Approach to Evaluate the Benefits of Casing Treatment in Axial Compressors

Table 5

Design features of the CBUAA [22].

Blade number	17
Tip diameter	355.8 mm
Design speed	22000 rpm
Hub-to-tip ratio	0.565
Aspect ratio	0.956
Mass flow at design point	13.4 kg·s^−1
Total pressure ratio at design speed	1.6 (stage)
Adiabatic efficiency at design speed	0.88 (stage)
Relative Mach number of tip rotor speed	1.404