Plane maker to automatically estimate the coefficients of lift (Cl), drag (Cd), and moment?

Question

Hello, 

I am a researcher working on a fixed-wing UAV project. I tried to get aerodynamic coefficients after modifying some wing parameters using the Plane Maker. Unfortunately, after I change the parameters, the coefficients could not be update automatically as documented in the Plane Maker manual (as shown in the following picture)

I really hope it could help me to estimate the coefficients automatically right after I change a wing's parameter. Could you please help me out please? 

I am looking forward to your reply.

Thank you.

 

Answer 1

Can you please provide more information?

What version of Plane Maker are you using? What exact steps or boxes do you fill in to see this?