2D NACA0015 aerodynamic coefficients computimg -- CFD Online Discussion Forums

April 29, 2011, 09:29	2D NACA0015 aerodynamic coefficients computimg	#1
sailor New Member qingkai Join Date: Apr 2011 Posts: 11 Rep Power: 15	Hi, I'm fresh in Fluent. I have an easy question here. I want to get the aerodynamic coefficients of NACA0015 airfoil. But the results do not match with the data of others. So I need some help about the set in Fluent, such as choose Laminar or Spalart-Allmaras？steady or unsteady? Thanks in advance!

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