Table 4 Performance parameters at 97% blade span and 1.7% tip clearance for different cases.

From: Enhancement of aerodynamic performance of axial compressors utilizing natural aspiration through optimized casing circumferential slot

Case study

Efficiency

Total pressure loss coeff

Incidence (deg)

Loading factor

Plane (no treatment)

81.02%

3.06%

\(2.9\)

0.54

Initial aspiration slot

82.30%

1.90%

\(2.5\)

0.52

Optimized aspiration slot

84.5% (2.6%)

1.46% (− 14%)

\(2.4\)(− 3.4%)

0.51 (− 1.8%)