Buckling of the fuselage skin in an aircraft can be delayed by increasing the internal pressure. When the internal pressure is increased, it provides additional outward force on the fuselage skin, thereby enhancing its ability to withstand compressive loads and delaying the onset of buckling. This is because the increased internal pressure opposes buckling by applying a stabilizing stress.
To understand this concept, consider the relationship between buckling and pressure:
Thus, increasing internal pressure is an effective way to delay skin buckling.
A two-cell wing box has wall thickness 1.5 mm and shear modulus \(G = 27\ \text{GPa}\). A torque of 12 kNm is applied. Determine the shear stress in wall AD (round off to one decimal place). 