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Please check the slides and video from the 2022 workshop. https://dafoam.github.io/mydoc_workshops.html |
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Right, the tutorial does not include structural weight. But it does have skin thickness (constant t=3 mm). The skin, ribs, and spar thicknesses are not design variables and remain constant during optimization. The message you posted is a warning, not an error. |
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When I completed the Aerostructural Mach tutorial wing in the tutorial, I couldn't find the optimized bdf file and didn't know how to view the stress cloud map and skin thickness of the optimized wing.
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