EFFECTS OF STREAM SURFACE INCLINATION ON TIP LEAKAGE FLOW-FIELDS IN COMPRESSOR ROTORS

Experimental and computational results of tip leakage flow fields in a diagonal flow rotor at the design flow rate are compared with those i n an axial flow rotor. In the diagonal flow rotor, the casing and hub walls are inclined at 25 deg and 45 deg, respectively, to the axis of rotation, and the blade has airfoil sections with almost the same tip solidity as that of the axial flow rotor. It is found out that ''break down'' of the tip leakage vortex occurs at the aft part of the passage in the diagonal flow rotor. The ''vortex breakdown'' causes significa nt changes in the nature of the tip leakage vortex: disappearance of t he vortex core, large expansion of the vortex, and appearance of low r elative velocity region in the vortex. These changes result in a behav ior of the tip leakage flow that is substantially different from that in the axial flow rotor: no rolling-up of the leakage vortex downstrea m of the rotor, disappearance of the casing pressure trough at the aft part of the rotor passage, large spread of the low-energy fluid due t o the leakage flow, much larger growth of the casing wall boundary lay er, and considerable increase in the absolute tangential velocity in t he casing wall boundary layer. The vortex breakdown influences the ove rall performance, also: large reduction of efficiency with the tip cle arance, and low level of noise.