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Solving Inviscid Compressible Flow

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Old   March 2, 2010, 09:56
Default Solving Inviscid Compressible Flow
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KGN
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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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Old   March 3, 2010, 00:57
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Hi someone please reply..
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Old   March 4, 2010, 00:23
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someone reply please...



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Old   March 5, 2010, 13:47
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Paul Garlick
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A good place to start is the rhoCentralFoam solver. This solves the Euler equations for compressible flow.

Take a look at the tutorial cases (LadenburgJet60psi for example) for details of how to apply the wall boundary conditions.
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