I'm new to Mathematica as this is the first class I've had to used it in my undergrad time as an aerospace engineer. Anyway, I have run into a problem that I can't figure out. I have created .STL's of a wing I have created in Solidworks. I can get them into Mathematica simply with the Import function but the model has 0 volume, as I understand .STL's are just shells. I need to convert this shell into a solid. I'm essentially looking for the opposite of ShellRegion. Additionally, I want to take a high number of cross section cuts and calculate the moment of inertia about the axis perpendicular to the load and parallel to the plane I'm looking at. And area as well. I don't really understand meshes, so that could be an issue. Any help would be appreciated. ScreenShot
Link to STL: https://drive.google.com/file/d/1KEAaYLg_sMR67InfDEs12HpnzTGjysQf/view?usp=sharing
M = RepairMesh[Import["ExampleData/spikey.stl"]]
andTriangulateMesh[ BoundaryMeshRegion[MeshCoordinates[M], MeshCells[M, 2, "Multicells" -> True]]]
might help. $\endgroup$