When a complete fuselage ring, symmetrical about the ZZ axis, is under the action of a symmetrical loading system—the ring ABCD in FIG. 3.01 is one such example—it can be treated in two halves built-in at D and cut at B, in the manner described earlier.
The Analysis of Fuselage Frames
Solution by the Elastic Centre Method of Problems in the Design of Built-in Frames and Complete Fuselage Rings
Aircraft Engineering and Aerospace Technology ; 24 , 3 ; 76-80
01.03.1952
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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