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how to get exact vale of lift/drag coefficient |
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January 31, 2010, 14:16 |
how to get exact vale of lift/drag coefficient
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#1 |
New Member
saurabh deshpande
Join Date: Jan 2010
Posts: 4
Rep Power: 16 |
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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January 31, 2010, 16:44 |
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#2 |
New Member
Khor Yee Shin
Join Date: Jan 2010
Location: Glasgow UK
Posts: 6
Rep Power: 16 |
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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January 31, 2010, 23:48 |
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#3 |
New Member
saurabh deshpande
Join Date: Jan 2010
Posts: 4
Rep Power: 16 |
Thanks man. your suggestion helped.. i got it. thanks again!!
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