Research Article
Investigation of Performance and Rotor Tip Flow Field in a Low Speed Research Compressor with Circumferential Groove Casing Treatment at Varying Tip Clearance
Figure 9
Time-resolved casing static pressure over rotor for SolidWall and Groove at = 1.2% (a, b) and = 2.5% (c, d). SolidWall operating points are near stall, Groove operating points identical to SolidWall.