2D Airfoil & Wing solving with Fluent
I just need need some help here in a specific problem ...
I`m still new using Fluent and nowadays i will start learn how can i complete 2D Airfoil & Wing solving with Fluent and really searching about PDF or any web site give me all details for this issue
Exactly what i confused in :-
1- what is Initial Condition need to but it
2- how can but the boundary co.
3-what is the inlet data i need to input it in fluent
4-what is the result i need to take from fluent Cl Cd Cm.. just this ?
i will be wait ASAP for helping me about all of this
Thanks A lot
Dear Ahmed Shawky,
Please googling, "2d simulation airfoil" or "fluent simulation airfoil", you will see abundant of PDF which teaching on how to set up the Fluent for airfoil simulation.
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