International Journal of Rotating Machinery / 2013 / Article / Fig 7

Research Article

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

Figure 7

(a) contours on the pressure surface of the blade with UF and SF for TC = 0 to 4, (b) contours on the suction surface of the blade with UF and SF for TC = 0 to 4.
490543.fig.007a
(a)
490543.fig.007b
(b)

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