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January 26, 2013, 05:28 |
Zeroth order interpolation
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#21 |
New Member
Lorenzo A. Ricciardi
Join Date: Mar 2011
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Hi all,
Is there a way to force a "flat" (i.e. zeroth order) cell to face interpolation using the above mentioned interpolate method? Thanks |
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January 31, 2013, 03:30 |
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#22 |
Senior Member
Mahdi Hosseinali
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What do you mean by flat cell? that would be against FVM definition of spatial discretization.
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January 31, 2013, 08:56 |
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#23 |
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Lorenzo A. Ricciardi
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"Flat" was relative to the interpolation, not to the cell. Call it constant interpolation (or zeroth order), if you prefer.
I don't agree with you about flat interpolation being against FVM. When you pass from a generic nonlinear hyperbolic equation like d/dt (u) + div(F(u)) = 0 // d is partial time derivative to a semi discrete form, you have to integrate on the cell volume. The div term becomes a surface integral, but (if the cell geometry is constant) the partial time derivative becomes the time derivative of a volume integral. The equation is divided by the volume of the cell, and you have an ODE for each cell averaged value. Thus each value is "flat" inside the cell. I'm implementing a particular solver in openFoam, which uses Riemann solvers, and although I will definitely use some kind of limited interpolation of values to the surface to get high resolution, for testing and completeness considerations I'm trying to use the unified "interpolate" function to assign a value from a volumeField to a surfaceField. I solved the problem with a very simple routine I've written from scratch, but it doesn't work in parallel so far: Code:
for (label faceI = 0; faceI < mesh.nInternalFaces(); faceI++) { label cellI = mesh.faceOwner()[faceI]; rho_neg[faceI] = rho[cellI]; U_neg[faceI] = U[cellI]; lambda_neg[faceI] = lambda[cellI]; label cellJ = mesh.faceNeighbour()[faceI]; rho_pos[faceI] = rho[cellJ]; U_pos[faceI] = U[cellJ]; lambda_pos[faceI] = lambda[cellJ]; } Thanks |
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January 31, 2013, 12:23 |
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#24 |
Senior Member
Mahdi Hosseinali
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I know how FVM works, what you want is piece wise constant while usually piece wise linear is being used. I believe you are going to use Gudonove type methods which still would yield a better result if you use piecewise linear rather than constant.
Anyway, there is a simple way to interpolate from vol<type>Field to surface<Type>Field, and that is fvc::interpolate, look it up in Doxygen. Also you might wanna take a look at the solver rhoCentralFoam, it is using what you are after. |
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January 31, 2013, 15:11 |
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#25 |
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Lorenzo A. Ricciardi
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I know Godunov method, and that's why I'm implementing another solver, different even from RhoCentralFoam
I'll try to look deeper inside Doxygen, thanks anyway |
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June 30, 2013, 08:48 |
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#26 | |||
Retired Super Moderator
Bruno Santos
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Greetings to all!
In reference to the following quotes, I believe that the missing link is this thread: http://www.cfd-online.com/Forums/ope...ow-solver.html The OpenFOAM Forum changed software a few times, so it's normal that some links are still broken Quote:
Quote:
Quote:
Bruno |
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August 26, 2013, 12:15 |
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#27 |
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Ehsan
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can anyone explain the lines or steps of rhoCentralFoam solver?
or a link or any instruction?
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December 24, 2013, 17:02 |
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#28 |
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Ehsan
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Hi all,
there is a link about density-based solvers in Fluent site:http://aerojet.engr.ucdavis.edu/flue...htm#ram-scheme that says all density-based solvers are coupled. does rhoCentralFoam solve equations in a segregated way or coupled way?
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December 28, 2013, 17:20 |
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#29 | ||
Retired Super Moderator
Bruno Santos
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Hi Ehsan,
Quote:
Quote:
Nonetheless, if you already have an overview of the equations being solved in rhoCentralFoam, it should be somewhat clear if it's segregated or coupled, from the way that the equations are solved: http://www.cfd-online.com/Wiki/Fluen...ated_solver.3F Best regards, Bruno
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April 15, 2014, 05:05 |
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#30 |
New Member
anshul bansal
Join Date: Jun 2013
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Hi...
can u please explain what means by these terms... rhoU ,rPsi, e, phiv, tauMC, sigmaDotU and phiEp... Thanks Anshul |
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April 16, 2014, 05:18 |
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#31 | |
Senior Member
Ehsan
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Quote:
rhoU=rho*U rPsi=R*T phiv=A*U (I have some doubt about it) phiEp=rho*A*U and two other terms are related to turbulence models and viscosity. definition of terms there are in solver codes.
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April 16, 2014, 06:19 |
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#32 |
New Member
anshul bansal
Join Date: Jun 2013
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hi..
thanks... here A= area or some other mean...?? and is there any description file where i can get these definition ?? Anshul |
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April 16, 2014, 07:50 |
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#33 |
New Member
anshul bansal
Join Date: Jun 2013
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ohh... i get this..
here A=rho*U means mass flow is is right.?? |
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April 16, 2014, 11:06 |
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#34 |
Senior Member
Ehsan
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A is the normal area of the cell to outside (inflow or outflow). unfortunately there is not a complete guide. phi in open foam is the mass flux and phiv is volumetric mass flux as I remember and is about incompressible problems.
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Injustice Anywhere is a Threat for Justice Everywhere.Martin Luther King. To Be or Not To Be,Thats the Question! The Only Stupid Question Is the One that Goes Unasked. |
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April 18, 2014, 16:04 |
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#35 |
New Member
anshul bansal
Join Date: Jun 2013
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hi immortality,
in rhoCentralFoam.c what mean by mesh.Sf() (in 105 line, openfoam 2.2.1 version) i attach this file thanks anshul |
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April 18, 2014, 16:33 |
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#36 | |
Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
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Quote:
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Injustice Anywhere is a Threat for Justice Everywhere.Martin Luther King. To Be or Not To Be,Thats the Question! The Only Stupid Question Is the One that Goes Unasked. |
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April 22, 2014, 15:20 |
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#37 |
New Member
anshul bansal
Join Date: Jun 2013
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hi immortality,
thanks for reply. i have another last doubt... which can help me very much. can u explain this sigmaDotU.... what this muEff and snGrad(U) ?? and this equation // --- Solve energy surfaceScalarField sigmaDotU ( ( fvc::interpolate(muEff)*mesh.magSf()*fvc::snGrad(U ) + (mesh.Sf() & fvc::interpolate(tauMC)) ) & (a_pos*U_pos + a_neg*U_neg) ); |
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August 20, 2014, 03:46 |
A little question: rhoCentralFoam implementation
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#38 |
Member
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Hi,
I'm trying to understand the implementation of rhoCentralFoam. I check the original paper of Greenshield, but I found some discrepancies between theory and implementation. in the attached document I explain my doubts. If anyone can help me, I'll be very thankful. Thanks in advance https://copy.com/1mcVjlWREUPt Felipe by the way if anyone want to try copy (better than dropbox!!) https://copy.com?r=HYM0VM
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Felipe G |
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August 6, 2015, 11:58 |
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#39 |
Senior Member
Freedom
Join Date: May 2014
Posts: 209
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Dear Luca and Alberto,
a = Grad(x-) = (PHI (i, j) - PHI(i-1, j))/ deltaX I have several questions about the upwind scheme:
Please help me..... Thank you very much!!! Best regards, Wen |
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November 5, 2015, 04:22 |
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#40 | |
Member
Xinguang Wang
Join Date: Feb 2015
Posts: 45
Rep Power: 11 |
Hi Felipe
I met the same situation, have you figure it out? Jason Quote:
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