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How can you realise and capture drag and lift coefficient for different angle of attack on an airfoil and plot them?

Question asked by Huy Khong Duc on Dec 21, 2015
Latest reply on Dec 28, 2015 by Danny Bouldin

Dear SolidWorks Community, this one is a real brain-teaser that I can't get my head around, so helps are really appreciated ^^. Thanks alot in advance.

I have an airfoil profile on which I would like to run ( and have been running) flow simulation to determine drag and lift coefficient. But know the tutor of this project is asking us to run simulation on different attack angles and plot the drag/lift curve.

Anyone knows how to do this automatically on SolidWorks?

 

Thanks very much. have a nice holiday!

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