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

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<iframe width="560" height="315" src="https://

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www.youtube.com/embed/3XBw_VRNLXU?si=wE9OlyqJSnPHxCPm" title="YouTube video player" frameborder="0" allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share" referrerpolicy="strict-origin-when-cross-origin" allowfullscreen></iframe>


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

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<iframe width="560" height="315" src="https://youtu.bewww.youtube.com/embed/xx65AsQU2Ic"><?si=ngVAc1fuQRVFlWWh" title="YouTube video player" frameborder="0" allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share" referrerpolicy="strict-origin-when-cross-origin" allowfullscreen></iframe>


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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