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Showing results 1 to 2 of 2 Search took 0.00 seconds. Search: Posts Made By: Martin Hegedus

Forum: OpenFOAM July 30, 2011, 22:06

Replies: 14 NACA0012: Residual convergence issue Views: 6,049 Posted By Martin Hegedus Lift curve slopes for airfoils will be higher... Lift curve slopes for airfoils will be higher than 2pi due to boundary layer thickness. I view it as the boundary layer creating an airfoil with a longer chord than the original. OK, not entirely...

Forum: OpenFOAM July 29, 2011, 15:42

Replies: 14 NACA0012: Residual convergence issue Views: 6,049 Posted By Martin Hegedus In regards to residual not converging: A... In regards to residual not converging: A short while ago we had a topic which included the airfoil2D which is under the simpleFoam tutorial directory. ...

Showing results 1 to 2 of 2

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