International Journal of Rotating Machinery / 2009 / Article / Tab 1

Research Article

Performance Improvement of Axial Compressors and Fans with Plasma Actuation

Table 1

Design parameters of the blades.

Tip Mach number0.5
Tip Radius0.3 m
Inlet hub-to-tip ratio0.70
Inlet absolute flow angle
Mid Span Solidity1.16
Aspect Ratio1.15
Mean Flow coefficient0.6
Inlet Total Pressure101300 Pa
Intel Total Temperature300 K

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