International Journal of Rotating Machinery / 2013 / Article / Fig 12

Research Article

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

Figure 12

End wall loss and flow deviation with reference to exit flow angle along the span in the wake with UF and SF for TC = 0.5 to 4.
490543.fig.0012

Article of the Year Award: Outstanding research contributions of 2020, as selected by our Chief Editors. Read the winning articles.