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 Thanks ... |
Re: Studying the span-wise load distribution of a
UP ;)
any ideas??? |
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