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What is the primary concern with a thin sheet-aluminum alloy in monocoque construction?

It does not provide strength

It is too heavy for flight

It must be designed to withstand stress and minimize weight

In monocoque construction, the primary concern with a thin sheet-aluminum alloy is that it must be designed to withstand stress while minimizing weight. This type of construction relies on the external skin to carry loads, which means that the material must possess sufficient strength to endure various forces, such as aerodynamic loads and internal pressures, without adding excessive weight that could compromise the performance of the aircraft.

Thin sheet-aluminum alloys can provide a good strength-to-weight ratio, but careful design and engineering are crucial to ensure that the structure can handle operational stresses. Therefore, emphasis on both strength and weight is vital in the design process when utilizing such materials in aviation applications. While other concerns like corrosion exist, they are secondary to the foundational requirement that the structure be strong yet lightweight.

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It is prone to corrosion

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