Effect of a Recirculating Type Casing Treatment on a Highly Loaded Axial Compressor Rotor

Abstract

The tip leakage flow over the blades of an axial compressor rotor adversely affects the axial rotor efficiency and can determine the onset of tip leakage stall. The performance of a new casing treatment concept in the shape of an axisymmetric recirculation channel is explored by steady Reynolds-Averaged Navier–Stokes (RANS) realizable k-ε modelling on the NASA Rotor 37 test case. The modelling exposed a number of attractive features. The casing treatment increased the stall margin at no penalty to the rotor isentropic efficiency over the rotor operating line. A recirculation in the casing channel self-activated and self-adjusted with the rotor loading to provide more passive flow control at higher rotor loading conditions. The nozzle-shaped recirculation channel outflow opposed the tip leakage jet, re-located the casing surface flow interface further downstream, and reduced the rotor blade tip incidence angle. This combination of features makes the new casing treatment particularly attractive for applications to high thrust-to-weight ratio engines, typical of high-performance jet aircraft.

Investigation of Vaned-Recessed Casing Treatment in a Low-Speed Axial-Flow Compressor, Part II: Unsteady Results

“…The favorable effect of the selfrecirculating casing treatment was found to be due to the weakening of the tip-leakage vortex/shock interaction and the formation of the tip-secondary vortex, which results in less blockage in the passage. A recirculating type casing treatment was tested in a highly loaded compressor by Kawase [40]. The stall margin improvement was found to be due to altering the interaction between the tip-leakage vortex and shock wave.…”