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Titlebook: Computerized buckling analysis of shells; D. Bushnell Book 1989 Kluwer Academic Publishers 1989 calculus.design.linearity.model.modeling.n

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Buckling of ring-stiffened shells of revolution,mit of the material. With creep neglected in the analysis the shell is predicted to buckle nonaxisymmetrically in a bifurcation mode with 12 circumferential waves. With creep included the predicted mode of failure is axisymmetric collapse.
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https://doi.org/10.1007/978-94-009-3277-7ith nontrivial prebuckling behavior. As was pointed out before, bifurcation from a nonlinear prebuckling state is of practical interest only in configurations with a great deal of symmetry. That is why the applications here all involve axisymmetrically loaded shells of revolution.
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Bifurcation buckling in which nonuniformity or nonlinearity of the prebuckling state is important,ith nontrivial prebuckling behavior. As was pointed out before, bifurcation from a nonlinear prebuckling state is of practical interest only in configurations with a great deal of symmetry. That is why the applications here all involve axisymmetrically loaded shells of revolution.
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0924-2112 their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a gene978-94-010-8741-4978-94-009-5063-4Series ISSN 0924-2112
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Imperfection sensitivity, test and bifurcation buckling theory, such as demonstrated in the extreme cases of the cylindrical shell under axial compression (Fig. 19) and the spherical shell under external pressure (Fig. 30). With the exception of the examples in the previous chapter involving modal interaction in axially com
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Book 1989ess of which is small com­ pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a gene
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