|May 28, 2013, 13:35||
simulation around an hydrofoil using simpleFoam - SA model
Join Date: Sep 2012
Posts: 1Rep Power: 0
I am trying to simulate a steady-state turbulent flow around a chord-normalized hydrofoil. The Reynolds number is Re = 10^6 and the angle of attack is set to 2deg.
I am using simpleFoam with the Spalart-Allmaras model. For the initial & boundary conditions, we need to define the eddy viscosity (nut) and the viscosity-like variable (nuTilda). My assumption is that the flow is laminar in the farfield, so I set the turbulent viscosity to zero at the inlet, outlet and on the top/bottom (symmetryPlane).
I also make the assumption that in the viscous sub-layer, the flow can be considered as laminar, and so, the eddy viscosity is set to zero.
To avoid refining the mesh so much, I also use a wall function "nutUSpaldingWallFunction".
My first question is: from which value of y+ do I have to use a wall function?
My convergence criteria are set to 10^-5 (see fvSolution file attached). However, the convergence is never reached. When I am plotting the drag and lift coefficients over the iterations, I have a lot of oscillations (see attached file). Even when I am refining the mesh, these oscillations are still here. Moreover, the convergence history looks very poor; my pressure residual is around 0.1 (see attached file).
Plotting the vorticity field, it looks like it is not well resolved (see attached file).
My second question: what is the best solver solution for the pressure for high Reynolds?
If you have any advice to give me, that will be very helpful!
Thank you very much.
|May 29, 2013, 06:47||
Join Date: Jul 2010
Location: Always on the move.
Posts: 308Rep Power: 8
1) SA is not really good for that flow regime, you will need more advanced turbulence models to have realistic results,
2) i'ts been a while since i used it but i don't think SA cope well with wall functions. you shuld fully define the viscous sublayer and have a y+ less than 1
3) check your mesh, i bet you have something horrible going on with the BL at approx 60-80% of the chord, on both sides of the foil
4) increase the residuals tolerance. for the pressure try GAMG
Naval architecture and CFD consultancy
|openfoam, simplefoam, spalart allamras, turbulence, wall function|
|Thread||Thread Starter||Forum||Replies||Last Post|
|SimpleFoam case with SpalartAllmaras turbulence model implemented||nedved||OpenFOAM Running, Solving & CFD||2||November 30, 2014 23:43|
|Turbulence Model in axisymmetric nozzle simulation||cric92||FLUENT||2||May 22, 2013 11:50|
|hydrofoil transient simulation||lingga hardiana||Main CFD Forum||0||July 25, 2012 04:58|
|Polyflow Simulation with ViscoElastic Model memory problem||sid2909||FLUENT||0||May 10, 2010 05:29|
|Polyflow Simulation with ViscoElastic Model memory problem||sid2909||ANSYS||0||May 10, 2010 05:27|