Performance Improvement of Axial Compressors and Fans with Plasma Actuation

Table 1

Design parameters of the blades.

Tip Mach number	0.5
Tip Radius	0.3 m
Inlet hub-to-tip ratio	0.70
Inlet absolute flow angle	0°
Mid Span Solidity	1.16
Aspect Ratio	1.15
Mean Flow coefficient	0.6
Inlet Total Pressure	101300 Pa
Intel Total Temperature	300 K