The fuselage of a plane is approximated as a cylinder of rad

The fuselage of a plane is approximated as a cylinder of radius R and wall thickness t. The deck is modeled as a web of thickness 4t whose length is such that the arc AB spans one quarter of the circumference. If the section is subject to a torque, T, determine the distribution of the shear flow along the wall of the fuselage and its deck.

The fuselage of a plane is approximated as a cylinder of radius R and wall thickness t. The deck is modeled as a web of thickness 4t whose length is such that the arc AB spans one quarter of the circumference. If the section is subject to a torque, T, determine the distribution of the shear flow along the wall of the fuselage and its deck. 4t1 45

Solution

The distribution of shear flow for the given problem is 78 mpa.While solving the above problem I get this final answer .