|
[Sponsors] |
November 7, 2014, 10:30 |
AUSM+ method at the sonic point
|
#1 |
Member
Ardalan
Join Date: Feb 2010
Location: Baku
Posts: 50
Rep Power: 16 |
I am solving 1d nozzle flow using ausm+ method
the results show a expansion shock at the throat (sonic point) Is this normal? by refining grid size, this unphysical shock diminishes. but in the paper figure, using the same number of meshes, there is not any jump at the throat. I'm really confused. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[snappyHexMesh] snappyHexMesh sticking point | natty_king | OpenFOAM Meshing & Mesh Conversion | 11 | February 20, 2024 09:12 |
On the alpha Eqn of VOF method when using Immersed boundary method in OpenFOAM | keepfit | OpenFOAM | 4 | January 31, 2014 14:32 |
[snappyHexMesh] snappyHexMesh and cyclic boundaries | Ruli | OpenFOAM Meshing & Mesh Conversion | 2 | December 9, 2013 06:51 |
[blockMesh] BlockMeshmergePatchPairs | hjasak | OpenFOAM Meshing & Mesh Conversion | 11 | August 15, 2008 07:36 |
[Gmsh] Gmsh and samplesurface | touf | OpenFOAM Meshing & Mesh Conversion | 2 | December 10, 2007 02:27 |