CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Running, Solving & CFD

Convergence problem with no slip BC simple foam- Actuator disk model

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   December 18, 2020, 09:56
Default Convergence problem with no slip BC simple foam- Actuator disk model
  #1
Member
 
Kabir Shariff
Join Date: Oct 2016
Location: France
Posts: 53
Rep Power: 9
Kbshariff is on a distinguished road
Hi foamers,

I am having trouble with residuals convergence when I used no slip wall BC in simple foam.

I am simulating a tidal turbine using actuator disc model defined in fvOption in OFv2006.

My case converges with slip walls at the bottom of the domain after say aroud 3000 iteration, but when I used no slip ( because i am using a log profile at inlet for U and I). the residual is still constant for 60,000 iterrations ( about 16 hrs runtime).

I attached herewith by case files please

U/

Code:
internalField   uniform (0 0 0);

boundaryField
{

    inlet           
   {
     type            groovyBC;
     variables (
		"zp=pos().z;"
		"a=0.197;"
		"u_f=0.00787;"
		"n=1e-6;"
		"vel=(2.5*u_f*log((u_f*zp)/(n))+a)*normal();"
		);
     valueExpression "-vel";

   }



    	outlet
    		{
       			type            zeroGradient;
    		}

	top
		{
			type		symmetry;
		}
	
	bottom
		{
			type		fixedValue;
			value		uniform (0 0 0);
		}

	walls
		{
			type		symmetry;
		}
"proc.*"
{
    type            processor;
}
	
}


p/

Code:
boundaryField
{

	inlet
		{
        		type           zeroGradient;
		}

    	outlet
    		{
       			type           fixedValue;
			value		uniform 0;
    		}

	top
		{
			type		symmetry; 	//zeoGradient;
		}
	
	bottom
		{
			type		zeroGradient;
		}

	walls
		{
			type		symmetry; 	//zeoGradient;
		}

"proc.*"
{
    type            processor;
}
k/

Code:
internalField   uniform 3.375e-4; //1.5*I_t^2*U_m^2

boundaryField
{
    inlet
    {
        type            groovyBC;
        variables	(
			"U_m=0.3;"
			"h=0.3;"
			"z0=0.001;"
			"I_t=0.05;"
			"r=pos().z/z0;"
			"I=I_t*((log(h/z0))/(log(pos().z/z0)));"
			);
	valueExpression	"1.5*pow(I,2)*pow(U_m,2)";
			
    }
    outlet
    {
        type            zeroGradient;
    }
    top
    {
        type		symmetry;			//type           kqRWallFunction;
        						//value          uniform 3.375e-4;
    }
    bottom
    {
        type            kqRWallFunction;
        		value           uniform 3.375e-4;
    }
    walls
    {
        type		symmetry;			//type           kqRWallFunction;
        						//value           uniform 3.375e-4;
    }

"proc.*"
{
    type            processor;
}
}


epsilon /
Code:
internalField   uniform 4.851e-5;

boundaryField
{
    inlet
    {
        type            fixedValue;
        value           uniform 4.851e-5;
    }
    outlet
    {
        type            zeroGradient;
    }
    top
    {
        type		symmetry;		//type           epsilonWallFunction;
        					//value          uniform 4.851e-5;
    }
    bottom
    {
        type            epsilonWallFunction;
        		value           uniform 4.851e-5;
    }
    walls
    {
        type		symmetry;		//type           epsilonWallFunction;
        					//value          uniform 4.851e-5;
    }

"proc.*"
{
    type            processor;
}
}

fvSchemes

Code:
ddtSchemes
{
    default             steadyState;
}

gradSchemes
{
    default             Gauss linear;
}

divSchemes
{
    default             none;

    div(phi,U)          bounded Gauss upwind;
    div(phi,epsilon)    bounded Gauss upwind;
    div(phi,k)          bounded Gauss upwind;

    div((nuEff*dev2(T(grad(U)))))    Gauss linear;
}

laplacianSchemes
{
    default             Gauss linear limited corrected 0.33;
}

interpolationSchemes
{
    default             linear;
}

snGradSchemes
{
    default             limited corrected 0.33;
}

fvSolution

Code:
solvers
{
    p
    {
        solver           GAMG;
        tolerance        1e-6;
        relTol           0.1;
        smoother         GaussSeidel;
    }

    U
    {
        solver           smoothSolver;
        smoother         GaussSeidel;
        tolerance        1e-6;
        relTol           0.1;
        nSweeps          1;
    }

    k
    {
        solver           smoothSolver;
        smoother         GaussSeidel;
        tolerance        1e-6;
        relTol           0.1;
        nSweeps          1;
    }

    epsilon
    {
        solver           smoothSolver;
        smoother         GaussSeidel;
        tolerance        1e-6;
        relTol           0.1;
        nSweeps          1;
    }
}

SIMPLE
{
    nNonOrthogonalCorrectors 0;

    residualControl
    {
        p               1e-3;
        U               1e-4;
        "(k|epsilon)"   1e-4;
    }
}

relaxationFactors
{
    fields
    {
        p               0.3;
    }
    equations
    {
        U               0.7;
        k               0.7;
        epsilon         0.7;
    }
}

cache
{
    grad(U);
}

Thank you!!!
Kbshariff is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
SU2-7.0.1 on ubuntu 18.04 hyunko SU2 Installation 7 March 16, 2020 04:37
error with reactingFoam BakedAlmonds OpenFOAM Running, Solving & CFD 4 June 22, 2016 02:21
Transition SST model - convergence problem with 2nd order discretization xara FLUENT 4 May 27, 2013 13:16
Convergence in Nat conv problem - simple geometry gradstudent2430 FLUENT 1 April 19, 2012 05:23
transition model convergence problem hammam CFX 3 August 7, 2007 18:33


All times are GMT -4. The time now is 16:00.