Orthogonality smoothing with ICEM CFD
I try to apply an othogonal smoothing on a structured hexahedral mesh (compressor blade), but it doesn't work efficiently. Is there anybody who have some good parameters to use to obtain the orthogonality near the walls. I tried to do as presented in this demo http://www.ansys.com/demoroom/zoom.aspx?d=11 but I obtain non orhogonal cells at the first layers close to the walls ...
Thank you very much by advance
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