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March 2, 2010, 08:56
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Solving Inviscid Compressible Flow
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#1 |
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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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March 2, 2010, 23:57
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#2 |
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Senior Member
KGN
Join Date: Oct 2009
Location: Chennai, India
Posts: 121
Rep Power: 16 |
Hi someone please reply..
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March 3, 2010, 23:23
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#3 |
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Senior Member
KGN
Join Date: Oct 2009
Location: Chennai, India
Posts: 121
Rep Power: 16 |
someone reply please...
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March 5, 2010, 12:47
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#4 |
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New Member
Paul Garlick
Join Date: Mar 2009
Location: Bournemouth, UK
Posts: 27
Rep Power: 17 |
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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