Studying the span-wise load distribution of a wing
Hello Fluent Users & Experts ;)
I was just wondering how easy or how feasible is it to make wing section cuts in Fluent?
I need to study the effects on the spanwise load distribution of the wing due to the cut....
any hints or relevant links would be much appreciated
Re: Studying the span-wise load distribution of a
|All times are GMT -4. The time now is 18:10.|