Search Results

Showing results 1 to 3 of 3
Search took 0.00 seconds. Search: Posts Made By: Farshad585

Forum: OpenFOAM Running, Solving & CFD

April 20, 2012, 13:13

Replies: 56

simpleFOAM NACA0012 (α=8°) cL, cD not matching published data

Views: 18,925

Posted By Farshad585

lift coefficient of NACA0012

Hi
I've used simpleFoam to analyze NACA0012 Airfoil with Angle of Attack 5 degrees. turbulence model is smalart-Allmaras. The lift coefficient is 0.476 after 5500 sec. the lift coefficient did not...

Forum: OpenFOAM Running, Solving & CFD

April 20, 2012, 12:54

Replies: 56

simpleFOAM NACA0012 (α=8°) cL, cD not matching published data

Views: 18,925

Posted By Farshad585

Thanks a lot

Thanks a lot

Forum: OpenFOAM Running, Solving & CFD

April 17, 2012, 17:53

Replies: 56

simpleFOAM NACA0012 (α=8°) cL, cD not matching published data

Views: 18,925

Posted By Farshad585

lift & drag coefficients

Hi
I'm a new user in OpenFOAM. I've run NACA0012 by using simpleFoam. I used a common file to compute lift and drag coefficients. but my lift and drag coefficients are too low. I think it is related...

Showing results 1 to 3 of 3

Forum Jump

All times are GMT -4. The time now is 19:05.