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Search: Posts Made By: vaina74
Forum: OpenFOAM Running, Solving & CFD March 30, 2010, 06:19
Replies: 5
Views: 2,356
Posted By vaina74
I know the lift (or drag) equation is: C_L=...

I know the lift (or drag) equation is:

C_L= \frac{L}{\frac{1}{2}{\rho}v^2A_{ref}}

where A_{ref} is planform area. In the section lift coefficient (based on the concept of an infinite wing of...
Forum: OpenFOAM Running, Solving & CFD March 29, 2010, 12:49
Replies: 5
Views: 2,356
Posted By vaina74
Thanks, Maddalena. First I merged all the threads...

Thanks, Maddalena. First I merged all the threads about lift and drag, then I found the nacaAirfoil tutorial (in compressible/sonicFoam/ras). I included in my controlDict:
functions
{
forces
...
Forum: OpenFOAM Running, Solving & CFD March 26, 2010, 07:57
Replies: 5
Views: 2,356
Posted By vaina74
forces on a hydrofoil

I included a subroutine in the controlDict file to evaluate the lift and drag coefficients on a blade section of a marine propeller:

functions
(
forces
{
type forces;
functionObjectLibs...
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