Page 477 - Aircraft Stuctures for Engineering Student
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458 Structural constraint
Fig. 11.14 Equilibrium of element of central boom.
Fig. 11 .I5 Equilibrium of a length z of cover.
We now consider the compatibility condition which exists in the displacements of
elements of the booms and adjacent elements of the panels. Figure 11.16(a) shows
the displacements of the cover and an element of a panel and the adjacent elements
of theboom. Note that the element of the panel is distorted in amanner which
Id shape
t
(a)
Fig. 11 .I6 Compatibility condition.
