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April 23, 2016, 04:33 |
Ansys Fluent NACA12 Meshing
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#1 |
Member
Shah
Join Date: Aug 2013
Posts: 61
Rep Power: 13 |
Hi Members
I am meshing flow domain around NACA12 but it is giving me tough time in Fluent. Well , the main disappointing is the edge sizing. I have imported the NACA in two , upper and lower, parts. I want to mesh the region around the airfoil based on the edge sizing. I want denser mesh at the leading and trailing edges. The mesh has to be triangular. The method that comes by default is On: curvature. But i dont know why choices for edges division is overridden. I cant figure how to resolve it ! Rescue !! |
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