enghelp2806
Aerospace
- Nov 16, 2020
- 16
How can I determine the thickness of a bolt plate, given the forces shown applied at the lug hole? I am fully aware of how to distribute the loads into each fastener, but then what? I know that the applied forces create (Mx, My, and Mz) moments as well as shear at the bolt group c.g. How can I relate those moments to the allowable strength of the plate? It seems easy enough to deal with the shear stresses, since those would just be the force in each direction divided by the shear area and then compared to the material shear strength.