Solving Inviscid Compressible Flow -- CFD Online Discussion Forums

March 2, 2010, 08:56	Solving Inviscid Compressible Flow	#1
mecbe2002 Senior Member KGN Join Date: Oct 2009 Location: Chennai, India Posts: 121 Rep Power: 16	Hi all, I am just started using OpenFoam and trying to solve Inviscid compressible flow around NACA0012 airfoil for Mach No=0.5 & alpha - 0. If i give "slip" boundary condition for airfoil, it will be treated as Inviscid wall and OpenFoam solves only Euler equation? please clarify

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