Balsa will be predrilled larger than the bolt diameter. The carbon will sandwhich around where the bolt hole will be. The hole will cut through only the carbon, leaving the balsa sandwhiched. The fastener will have a washer large enough to apply pressure to the sandwhiched balsa, not the carbon that is sandwiching the balsa. I wish I had a CAD program to draw it out, it would make a lot more sense than what I just wrote. Basically the balsa will not be cut, will remain sandwhiched on all sides and around the bolt hole, and the bolt/fastener will apply pressure to the balsa, not the carbon sandwiching it.
I've heard of mesh being used inter laminate, though I don't think it is very common. The reason that is in the tentative layup schedule, is because I do not know if the large pieces of balsa will allow resin to reach the fabric underneath it. Mesh will create a channel and allow the resin to flow under the balsa and fully saturate the laminate. I am going to layup a test panel with and without the mesh to determine if it is needed and if there is any noticeable structural differences to the panels. Being that it is sandwhiched and will be essentially a core, I don't see it causing any issues with delamination. But that is only my assumption and that is why I am doing the test panels first.
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