tailieunhanh - Aerodynamic performance of a single stage transonic axial compressor using recirculation bleeding channels

This paper investigates the recirculation channel with an addition of bleeding channels located on shroud surface of recirculation channel in the rotor domain, where the bleeding system consists of 36 channels distributed on the recirculation channel. | Aerodynamic performance of a single stage transonic axial compressor using recirculation bleeding channels