Cb. York et Fw. Williams, THEORY AND BUCKLING RESULTS FOR INFINITELY WIDE, STIFFENED SKEW PLATEASSEMBLIES, Composite structures, 28(2), 1994, pp. 189-200
Existing theory and the associated computer program VICONOPT deal with
infinitely wide plate assemblies given that boundary conditions on al
l sides of each panel form a rectangle. They also deal with cases when
the four supports form a parallelogram so that the plate is a skew pl
ate. This is true provided the panel is of finite width, i.e. isolated
from any adjacent panels, which is the case commonly modelled in prac
tice. It does not represent what happens in the real structure, howeve
r, where normally there is continuity with the adjacent panel. The pre
sent paper shows how the theory and the computer program VICONOPT can
be modified so that skewed plate assemblies that are infinitely wide a
nd repeat at transverse intervals can now be modelled exactly. The pap
er also shows that the theory can be used, if a small measure of appro
ximation is accepted, to model this situation by analysing only one of
the identical stiffeners with associated panel skin in the common sit
uations where the panel has equally spaced, identical, longitudinal st
iffeners between each adjacent pair of longitudinal lines of support.
Illustrative results are given.