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Old   September 14, 2005, 02:36
Default Clift,Cdrag
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DAK565656
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Hello! I am new in CFX. I obtained results from the flow over an airfoil. Please, how can I get Clift and Cdrag for this in CFX?
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Old   September 14, 2005, 03:42
Default Re: Clift,Cdrag
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alf
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You have the 6 components of the force (viscous and pressure in 3 directions) at the end of the job in the .out

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Old   September 14, 2005, 05:46
Default Re: Clift,Cdrag
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DAK565656
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If I want to count coefficients for specific body in the domain? To what body does these forces applied?
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Old   September 14, 2005, 07:01
Default Re: Clift,Cdrag
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DAK565656
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Of course. It is written in this file. No more questions... thanks
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