Ansys Fluent NACA12 Meshing -- CFD Online Discussion Forums

April 23, 2016, 03:33	Ansys Fluent NACA12 Meshing	#1
researcher Member Shah Join Date: Aug 2013 Posts: 61 Rep Power: 12	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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