Lift and drag coefficients of wing in incompressible flow

Using SimScale Fluid Flow / CFD
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Hello all,

I am having issues with the lift and drag coefficients. I have used the surface area from CATIA as well as the centre of rotation as the cog from CATIA. I am still getting values that are not right.

Please help.
Thanks

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Hi @moboluwarin_ma,

Thanks for posting your question! Could you please share the project link here? Just in order to speedup the support taking a close look at that one.

Thanks you very much,

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It turns out it was the conversion from mm to m from CATIA. It’s giving reasonable values now.
Thanks.