 |
 |
 |
|
|
|
[Sponsors] | ||||
March 2, 2010, 09:56
|
Solving Inviscid Compressible Flow
|
#1 |
|
Senior Member
KGN
Join Date: Oct 2009
Location: Chennai, India
Posts: 121
Rep Power: 18  |
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 |
|
|
|
|
|
March 3, 2010, 00:57
|
|
#2 |
|
Senior Member
KGN
Join Date: Oct 2009
Location: Chennai, India
Posts: 121
Rep Power: 18 |
Hi someone please reply..
|
|
|
|
|
|
|
March 4, 2010, 00:23
|
|
#3 |
|
Senior Member
KGN
Join Date: Oct 2009
Location: Chennai, India
Posts: 121
Rep Power: 18 |
someone reply please...
  |
|
|
|
|
|
|
March 5, 2010, 13:47
|
|
#4 |
|
New Member
Paul Garlick
Join Date: Mar 2009
Location: Bournemouth, UK
Posts: 27
Rep Power: 18 |
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. |
|
|
|
|
|
 |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Floating point exception error | Alan | OpenFOAM Running, Solving & CFD | 11 | July 1, 2021 22:51 |
| Computational time | sunnysun | OpenFOAM Running, Solving & CFD | 5 | March 16, 2009 04:32 |
| MRFSimpleFoam amp cyclic patches | david | OpenFOAM Running, Solving & CFD | 36 | October 21, 2008 22:55 |
| Convergence moving mesh | lr103476 | OpenFOAM Running, Solving & CFD | 30 | November 19, 2007 15:09 |
| why compressible flow solving isnt need energy Eqn | starPlatinum | Main CFD Forum | 1 | July 21, 2003 11:15 |
Linear Mode
