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.
490543.fig.003a
(a)
490543.fig.003b
(b)

We are committed to sharing findings related to COVID-19 as quickly and safely as possible. Any author submitting a COVID-19 paper should notify us at help@hindawi.com to ensure their research is fast-tracked and made available on a preprint server as soon as possible. We will be providing unlimited waivers of publication charges for accepted articles related to COVID-19.