✅💯✅ Ansys Fluent Project # 37 : CFD Analysis of Wing | Steady State

[@khalid26752]

Your videos are so great sir!
Im doing some cfd for f1 wings, and Im facing some troubles
I have a 3 elements wing, but I don't know how to calculate the planform area
Should I adjust all the 3 elements to zero AoA, then taking the planform area?
Or should I consider all the 3 elements as 1 indivisual wing and then taking the planform area?
And if I did the second choice, should the equvalent wing be in zero AoA or what??
Please let me know

[@keyvanhp5841]

please send a video about drag coefficient simulation of a soccer ball .