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NACA_0012_Airfoil.txt

The video at the link below shows you how to create the initial wing geometry in Ansys Discovery. 

https://youtu.be/3XBw_VRNLXU

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The video The video at the link below shows you how to set up the initial wing analysis in Ansys Mechanical. 

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Reiterate with varying numbers of spars/ribs, varying locations, and different thicknesses. For optimizing thickness, you can use Response Surface Optimization. This tutorial should help:

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