Abstract
This paper uses perturbation techniques in asymptotic procedures to determine the normal displacement, the associated Airy stress function and the dynamic buckling load of an imperfect, finite toroidal shell segment pressurized by a step load. The adoption of asymptotic and perturbation procedure is made possible by the presence of small non-dimensional parameter on which asymptotic expansions are made possible. It is assumed here that the imperfection can be regarded as the first term in the Fourier Sine series expansion. The buckling modes are also assumed to be strictly in the shape of the imperfection which is in turn given in the shape of the classical buckling mode. In the final analysis, a simple but implicit formula for determining the dynamic buckling load was obtained. The dynamic buckling load was related to the corresponding static buckling load and that relationship is independent of the imperfection parameter. It is observed, that this procedure, perhaps more than other ones, can be used to analyze relatively more complicated problems particularly where more demands and restrictions are placed on the imperfection parameter. The results are strictly and are valid as far as the imperfection parameter is relatively small compared to unity.
Highlights
An elastic toroidal shell segment is one of the most imperfection–sensitive structures in Structural Mechanics, yet, little seems to be known about its dynamic stability when subjected to time dependent loads
We shall aim at deriving an implicit formula for evaluating the dynamic buckling load of the structure assuming that it is pressurized by a step load
The work intends to relate the dynamic buckling load to the corresponding static buckling load and that relationship is independent of the imperfection parameter
Summary
An elastic toroidal shell segment is one of the most imperfection–sensitive structures in Structural Mechanics, yet, little (to our knowledge) seems to be known about its dynamic stability when subjected to time dependent loads. Unlike cylindrical shells which it shares some form of semblance of structural similarity, investigations probing into the dynamic behavior of toroidal shell segments appear to be rather scanty. In this investigation, our aim is to explore the deformation, in terms of the normal displacement and Airy stress function, of a finite imperfect toroidal shell segment pressurized by a step load. The aim of this work is to use regular perturbation technique and asymptotic expansion of the relevant variables to determine the normal displacement, the associated Airy stress function and the dynamic buckling load of an imperfect, finite toroidal shell segment pressurized by a step load. The work intends to relate the dynamic buckling load to the corresponding static buckling load and that relationship is independent of the imperfection parameter
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