Learning Forum

[bilal ojaily]

Hi! 

I am studing on wing to calculate CL and CD in different angle of attack, and I heard there is a method (parametric solution) like a loop to calculate it by changing angle of wing or velocity vector

how can I use this method?

[Rob]

By setting a parameter to alter the geometry (less efficient) or inlet velocity components (more efficient). However, read through the NACA examples in Help (tutorial and/or video) as force and coefficient reporting is a little less trivial.