Boundary Condition For a Transonic Wing -- CFD Online Discussion Forums

September 19, 2011, 05:51	Boundary Condition For a Transonic Wing	#1
morteza08 Senior Member Morteza Join Date: May 2010 Location: Iran,Islamic Republic of Posts: 161 Rep Power: 15	Hi all I am modeling a 3d wing in Gambit and Fluent in Transonic regime. I have a question about what B.C is more appropriate for front,back,top,bottom and sides of the computational domain? And what turbulence model will predict the best values for Cd and Cl and shock- boundary layer interaction? How much the boundaries of domain can be far from the domain? Thank you

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