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forceCoeffs in simpleFoam for and airfoil

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Old   June 7, 2012, 04:31
Exclamation forceCoeffs in simpleFoam for and airfoil
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Hi everyone,

I am learning how to get Cl and Cd coefficients from a simpleFoam simulation . I added the following part to my controlDict file
PHP Code:
type forces;
functionObjectLibs (""); //Lib to load
patches (wall); // change to your patch name
rhoName rhoInf;
rhoInf 1.006//Reference density for fluid
CofR (-0.004 0); //Origin for moment calculations
outputControl   timeStep;
outputInterval  1;
// rhoInf - reference density
// CofR - Centre of rotation
// dragDir - Direction of drag coefficient
// liftDir - Direction of lift coefficient
// pitchAxis - Pitching moment axis
// magUinf - free stream velocity magnitude
// lRef - reference length
// Aref - reference area
type forceCoeffs;
functionObjectLibs ("");
patches (wall);
rhoName rhoInf;
rhoInf 1.006;
CofR (-0.004285 0);
liftDir (0 1 0);
dragDir (1 0 0);
pitchAxis (0 0 1);
magUInf 67;
lRef 1
Aref 1;

outputControl   timeStep;
outputInterval  1;

the problem is that I am getting a file with 2000 values of each coefficient!! I don't know how to get the final one ? can someone please help me
Attached Files
File Type: txt forceCoeffs.txt (80.3 KB, 35 views)
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Old   June 7, 2012, 05:04
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You are getting a value for every iteration. You may want to average the last iterations. I would pick at least the last 500 iterations.
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