Lift, drag and momentum coeff???
 

hello forum,

i have a 2d NACA-profile. i'm using the simpleFoam solver and i would like to obtain the lift, drag and momentum coefficients.

how can i obtain them?

best,
Ovidiu

problem solved
 

hello,

problem solved.

http://www.cfd-online.com/Forums/ope...efficient.html


best,
Ovidiu