Spanwise lift distribution on 3D wing
 

Hi,

I'm currently using Fluent and I'd like to carry out a spanwise lift analysis.

But the only thing I manage to do is a Cp analysis along the wing... (using the XY plot function). By any chance, is there a function to plot Cl in function of the spanwise location ?

Sorry, it's seem basics function, I obviously had a look at the user manual and other tutorials, but I haven't find anything !!!

Thanks for your help

Best regards

Fabrice

Re: Spanwise lift distribution on 3D wing
 

please help me, I do need this lift distribution in order to end my MSc thesis .... :)

Thanks for any kind of help