OpenFOAM Sample-Files



AeroFoam (Special Thanks to FreeCASE!!)
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

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


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


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


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


Ex4

Mach=5
P=1[Pa]
T=1[K]

none for OpenFOAM-1.4.1 sample-image::
solved by rhopSonicFoam
(check tutorial-case)









inserted by FC2 system