Wing Cl calculation
Hi i am using ansys fluent for CFD and i have successfully done 2D airfoil analysis.. but i am not able perform proper meshing of the 3D wing. And also i would like to know about its general process!
I wanted to calculate the wings coefficient of lift , drag, and center of pressure.
I am also interested in this question, and I think more people watching this webside is wondering it too.
Thank you in advance
|All times are GMT -4. The time now is 07:41.|