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Aerospace
Does anyone know how to calculate the stress concentration for a hole in the radius under axial loading?
My best guess is that it is a compound K(t)....one for the open hole and the other deriving from the equivalent of a shoulder fillet (from Peterson's).
Any input would be helpful.
My best guess is that it is a compound K(t)....one for the open hole and the other deriving from the equivalent of a shoulder fillet (from Peterson's).
Any input would be helpful.