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How does cfd package like fluent calculate parasite drag and induced drag?

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Old   July 28, 2023, 10:08
Default How does cfd package like fluent calculate parasite drag and induced drag?
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bella lau
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Hello everyone,

I am a newcomer to CFD and have encountered some questions regarding the calculation of induced drag and parasitic drag while using Fluent for simulations. I am wondering if Fluent allows direct output of induced drag and parasitic drag, but it seems that this feature is not available.

I have learned that Fluent can export the lift coefficient CL and the drag coefficient CD. I am curious if we can calculate the induced drag coefficient CDi using the equation : CDi = CLČ / (π * e * AR)(Where CL is the lift coefficient, e is the span efficiency factor and AR is the wing aspect ratio), and then use the equation : CD = CD0 + CDi to obtain the parasitic drag coefficient CD0?

I'm really looking forward to hearing from experienced members!

Thank you all!
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Old   July 28, 2023, 20:48
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No need for complicated empirical formula.

Fluent does output induced and parasitic drag. Induced drag is nothing but the projection of the lift force.
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Old   August 2, 2023, 08:54
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How can I achieve that?
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