Stressed skin

The Zeppelin-Lindau D.I had stressed skin fuselage and wings.

In mechanical engineering, stressed skin is a rigid construction in which the skin or covering takes a portion of the structural load, intermediate between monocoque, in which the skin assumes all or most of the load, and a rigid frame, which has a non-loaded covering. Typically, the main frame has a rectangular structure and is triangulated by the covering; a stressed skin structure has localized compression-taking elements (rectangular frame) and distributed tension-taking elements (skin).


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