International Journal of Rotating Machinery / 2013 / Article / Fig 3

Research Article

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

Figure 3

(a) Plan view of the wind tunnel test section with shear generator. (b) Multiblock structured mesh with the “O” grid around the airfoil and triangular prism mesh in the tip region only.

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