The fuselage of a plane is approximated as a cylinder of radius R and wall thick

Question

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

Explanation / Answer

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

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