3DPrinting
3DPrinting is a place where makers of all skill levels and walks of life can learn about and discuss 3D printing and development of 3D printed parts and devices.
The r/functionalprint community is now located at: [email protected] or [email protected]
There are CAD communities available at: [email protected] or [email protected]
Rules
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No bigotry - including racism, sexism, ableism, homophobia, transphobia, or xenophobia. Code of Conduct.
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Be respectful, especially when disagreeing. Everyone should feel welcome here.
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No porn (NSFW prints are acceptable but must be marked NSFW)
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If you see an issue please flag it
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The optimal structure is highly dependent on the type of loading: tension, compression, bending, shear, torsion, or combinations thereof. Thus, the results of these experiments are only valid for compression. For other load cases one either needs to do the specific experiments or run a topology optimisation, by e.g. a SIMP algorithm.
Or even in compression… if he had tested them with the weight moving along the printed z-axis.
Rectilinear, grid, lines, honeycomb and stars and any other patterns like that aren’t going to be the same.
Also, things change again with part geometry- some paterns won’t be able to set up that neat crushing pattern on something like the wing he had in an example.
Edit: if he had included solid top and bottom layers as well- which is probably more typical of printing- the attached infil would behave differently.