OpenFOAM Sample-Files
title | View | movie | SampleFile | comment |
Ex1 Mach=3 P=0.1[MPa] T=293.15[K] |
YouTube | for OpenFOAM-1.4.1 | sample-image:: solved by sonicFoam |
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Ex2 inlet :: Mach=0.22 P=0.1[MPa] T=288.15[K] |
none | for OpenFOAM-1.4.1 supersonicInlet extrapolatedOutlet for OpenFOAM-1.4.1 pressureInletOutletVelocity waveTransmissive |
check :: "Computational Methods for Fluid Dynamics" , J.H.Ferziger and M.Peric / Springer sample-image:: solved by sonicFoam |
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Ex3A Subsonic :: Min=0.5 |
none | for OpenFOAM-1.4.1 | check :: "Computational Methods for Fluid Dynamics" , J.H.Ferziger and M.Peric / Springer sample-image:: solved by sonicFoam |
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Ex3B Transonic :: Min=0.675 |
none | for OpenFOAM-1.4.1 | check :: "Computational Methods for Fluid Dynamics" , J.H.Ferziger and M.Peric / Springer sample-image:: solved by sonicFoam |
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Ex3C Supersonic :: Min=1.65 |
none | for OpenFOAM-1.4.1 | check :: "Computational Methods for Fluid Dynamics" , J.H.Ferziger and M.Peric / Springer sample-image:: solved by sonicFoam |
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Ex4 Mach=5 P=1[Pa] T=1[K] |
none | for OpenFOAM-1.4.1 | sample-image:: solved by rhopSonicFoam (check tutorial-case) |