Question: A fuselage cross section has been approximated to the hexagonal shape shown in the Figure below, for the sake of preliminary stress analysis. The load

A fuselage cross section has been approximated to the hexagonal shape shown in the Figure
below, for the sake of preliminary stress analysis. The load case being analyzed is of a 5000 N
shear force applied parallel to the left side of the hexagon, at station 0. The length of each of the
six sides of the cross-section is 1000 mm and the wall thickness is of 1 mm . Determine the
maximum normal stresses on a cross section 3000 mm behind station 0.
Thin walled monocoque hexagonal fuselage section subjected to a shear force
do not use CHATGPT
A fuselage cross section has been approximated to

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