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how to get exact vale of lift/drag coefficient

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Old   January 31, 2010, 13:16
Post how to get exact vale of lift/drag coefficient
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saurabh deshpande
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Hi everyone,

I am a beginner in the field of CFD. currently analyzing flow around an airfoil at different angles of attacks using FLUENT.

I want to plot graph of 'lift/drag coefficient' vs 'angle of attack'. But i don't know how to get exact value of lift/drag coefficient.

From the graph of 'lift coefficient vs iterations' i do get some idea about its value but not the exact value.

Please help. Thanks in advance
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Old   January 31, 2010, 15:44
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Khor Yee Shin
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You can get the values from the main console if you select the right settings (should be by default) . Check Solve --> Monitors --> Force ... then under lift and drag, make sure the option 'Print' is checked besides 'Plot'. The values should be 'printed' in the main console as the iteration is underway.
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Old   January 31, 2010, 22:48
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saurabh deshpande
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Thanks man. your suggestion helped.. i got it. thanks again!!
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