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How to find lift coefficient by fluent?

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June 3, 2009, 12:39	How to find lift coefficient by fluent?	#1
winterboy New Member Pooya Kabiri Join Date: Jun 2009 Posts: 1 Rep Power: 0	Hi everybody, I used fluent to model flow around NACA 0015. I got cl & Cd for the same flow and airfoil from Xfoil and want to compare Xfoil results with fluent results. I want to find Cl and Cd by fluent and my problem is the numbers which I have to enter for X,Y,Z of force vector. do you know what should I put in there and how many iterations should I have at least to get acceptable answer for Cl and Cd? Thank you in advance vivek_9894 and mehmed like this.

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Posted By	For	Type	Date
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