Research Article

Study of Sweep and Induced Dihedral Effects in Subsonic Axial Flow Compressor Passages—Part II: Detailed Study of the Effects on Tip Leakage Phenomena

Figure 7

Flow scenario for UNS rotor near the tip showing leakage flow, blockage with leakage vortex, and wake effect.
491413.fig.007a
(a) /ch = 0.7%
491413.fig.007b
(b) /ch = 2.7%