Which statement is true regarding cantilever wings?

Cantilever wings are designed to bear loads and resist bending without the need for external supports or bracing. This design effectively integrates the wing structure directly into the fuselage or body of the aircraft, utilizing materials and engineering techniques that allow the wing to support itself. This self-supporting characteristic is fundamental to the cantilever design, making it a preferred choice in modern aircraft construction, as it allows for a cleaner aerodynamic profile with fewer drag-inducing components.

While other designs may indeed require external bracing or supports, the cantilever wing's architecture relies on its internal structural capabilities, which can handle the aerodynamic and mechanical stresses encountered during flight. This means that the statement about the lack of need for external bracing accurately captures the essence of cantilever wing design and functionality.