International Journal of Rotating Machinery / 2013 / Article / Fig 14

Research Article

Investigation of the Shear Flow Effect and Tip Clearance on a Low Speed Axial Flow Compressor Cascade

Figure 14

Interaction of TLV (tip leakage vortex), IEV (induced end wall vortex), and TLF (tip leakage flow) with UF and SF at 1% and 4% tip clearance. Total pressure loss contours are used.
490543.fig.0014

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