Question: A fuselage thin wall cross section of circular shape ( Figure below ) is being analyzed for stresses under the effect of a 5 0

A fuselage thin wall cross section of circular shape (Figure below) is being analyzed for stresses under the effect of a 5000 N shear force applied parallel to the left side of the section, at station 0. The diameter of the cross-section is 2000 mm and the wall thickness is of 1 mm .
a) Determine the maximum normal stresses on a cross section 3000 mm behind station 0.
b) Obtain the shear flow around the section
Thin walled monocoque circular fuselage section subjected to a shear force
do not use CHATGPT
A fuselage thin wall cross section of circular

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