Comments on effective use of numerical modelling and extended classical shell buckling theory (original) (raw)

2023, Proceedings of The Royal Society A: Mathematical, Physical and Engineering Sciences

2. Extended classical shell buckling theory A number of reviews [31-34] have covered some of the background and important applications of the RS extension to classical shell buckling theory. These have demonstrated that for wide ranges of shell forms and loading conditions, the lower limits to the reductions in buckling loads caused by increasing levels of geometric (and loading) imperfections are provided by RS analysis, including the treatment of the development of material failure [6,31-33]. The philosophical basis of the RS method can be formulated [34] in terms of the following lemmas: Lemma 2.1. Significant geometric nonlinearity in structural behaviour results from changes in incremental membrane energy (or equivalently membrane stiffness). Corollary 2.2. Significant nonlinearity in the buckling of shell and plate structures derives from changes in incremental membrane energy. Corollary 2.3. Nonlinearity arising from changes of incremental bending energy is practically negligible. Lemma 2.4. Loss of stiffness (or load carrying capacity) in the buckling 1 and postbuckling (see footnote 1) of shells is the result of loss of incremental membrane energy. Corollary 2.5. Loss of stiffness (or load carrying capacity) in the postbuckling of shells can only occur if the initial buckling mode (critical bifurcation mode) contains membrane energy. Corollary 2.6. Loss of stiffness (or load carrying capacity) resulting from changes of incremental bending energy in the postbuckling of shells is practically negligible.

Towards a rationally based elastic-plastic shell buckling design methodology

Thin-Walled Structures, 1995

The 'reduced stiffness method' for the analysis of shell buckling was developed to overcome a trend towards increasingly sophisticated analysis that has become divorced from its basically simple underlying physics. This paper outlines the developments of the reduced stiffness method from its origins in the late 1960s, through its experimental confirmation, generalisation and elaboration over the past 20 years, to its more recent consolidation using carefully controlled non-linear numerical experiments. It is suggested that the method has now reached a stage where it could profitably be adopted as a basis for an improved shell buckling design methodology.

On Introducing Imperfection in the Non-Linear Analysis of Buckling of Thin Shell Structures

This master thesis details the investigation of the effect of geometrical imperfection on thin shell structures using general FEM software packages. The author proposes a finite element based method for the analysis and design of thin shell structures, and describes the implementation of such a procedure on four FEM packages. The procedure involves assessing structural imperfection sensitivity, and imposing geometrical imperfection prior to a physical and geometrical non-linear analysis.

Buckling of thin shells: Recent advances and trends

This paper provides a review of recent research advances and trends in the area of thin shell buckling. Only the more important and interesting aspects of recent research, judged from a personal view point, are discussed. In particular, the following topics are given emphasis: (a) imperfections in real structures and their influence; (b) buckling of shells under local/non-uniform loads and localized compressive stresses; and (c) the use of computer buckling analysis in the stability design of complex thin shell structures.

Numerical Methods for Determining the Dynamic Buckling Critical Load of Thin Shells. State of the Art

The Bulletin of the Polytechnic Institute of Jassy, Construction. Architecture Section, 2012

The problem of dynamic stability is substantially more complex than the buckling analysis of a shell subjected to static loads. The fundamental aim of this paper is to present criteria for determining the critical load of dynamic buckling of thin shell. Another purpose of establishing such criteria is to guide engineers scientists and researchers dealing with such problems, for a better comparison verification and a validation of their experimental or numerical results. To illustrate the application of these criteria, two examples have been studied.

Non-linear lower bounds for shell buckling design

Journal of Constructional Steel Research, 1994

Based on rigorous parametric non-linear elastic buckling analyses, the present work underlines the developments towards theoretical lower bounds of existing experimental buckling loads for some of the most practical shell geometries and loading cases, namely circular cylindrical shells under external pressure and~or axial loads and spherical caps under external pressure. Simple equations and formulae are presented and their predictions for buckling loads are compared with available test results and values prescribed by some of the existing design codes. These explicit lower bounds are close and non-conservative estimates of buckling loads of imperfect shells and as such are proposed as a consistent and rational basis for design of these shell structures.

Relaxation oscillations and buckling prognosis for shallow thin shells

Zeitschrift für angewandte Mathematik und Physik, 2020

This paper reports the possibilities of predicting buckling of thin shells with nondestructive techniques during operation. It examines shallow shells fabricated from high-strength materials. Such structures are known to exhibit surface displacements exceeding the thickness of the elements. In the explored shells, relaxation oscillations of significant amplitude could be generated even under relatively low internal stresses. The problem of cylindrical shell oscillation is mechanically and mathematically modeled in a simplified form by conversion into an ordinary differential equation. To create the model, works by many authors who studied the geometry of the surface formed after buckling (postbuckling behavior) were used. The nonlinear ordinary differential equation for the oscillating shell matches the well-known Duffing equation. It is important that there is a small parameter before the second time derivative in the Duffing equation. This circumstance enables a detailed analysis of the obtained equation to be performed and a description to be given of the physical phenomena-relaxation oscillations-that are unique to thin high-strength shells. It is shown that harmonic oscillations of the shell around the equilibrium position and stable relaxation oscillations are defined by the bifurcation point of the solutions to the Duffing equation. This is the first point in the Feigenbaum sequence at which stable periodic motions are converted into dynamic chaos. The amplitude and period of the relaxation oscillations are calculated based on the physical properties and the level of internal stresses within the shell. Two cases of loading are reviewed: compression along generating elements and external pressure. It is emphasized that if external forces vary in time according to the harmonic law, the periodic oscillation of the shell (nonlinear resonance) is a combination of slow and stick-slip movements. Because the amplitude and the frequency of the oscillations are known, this fact enables an experimental facility to be proposed for prediction of shell buckling with nondestructive techniques. The following requirement is set as a safety factor: maximum load combinations must not cause displacements exceeding the specified limits. Based on the results of the experimental measurements, a formula is obtained to estimate the safety against buckling (safety factor) of the structure.

A comparison of techniques for computing the buckling loads of stiffened shells

Computers & Structures, 1993

Abatraet-Three different methods are employed to estimate the buckling loads of several ring stiffened and orthotropic cylindrical shells using finite elements. The methods used are a nonlinear bifurcation analysis and two linearized buckling analyses, one that ignores the initial displacement stiffness matrix, and one that includes it. Large differences are observed between the predictions made by the two linearized buckling analyses for a range of shell geometries. Detailed studies of a shell with six stiffeners demonstrate that them differences am caused by different versions of the linearized eigenvalue problem, rather than by the use of different numerical formations. These diserepaneies are also observed for orthotropic shells when L/R is small (< 1) and the degree of orthotropy (EJE,) is high (2 10). Investigations of the prebuckling behavior of some of the cylinders show that the problem is caused by significant nonlinear pmbuckling deformations. This means that a nonlinear bifurcation analysis must sometimes be used to accurately estimate the buckling load of stiffened shells.

Buckling Load of Thin Spherical Shells Based on the Theorem of Work and Energy

International Journal of Engineering and Technology, 2013

Thin spherical shells usually fail due to buckling. An empirical equation to predict their buckling load is derived based on the theorem of work done and energy released in the inversion of a section of a shell and nonlinear finite element (FE) modeling done using ABAQUS to determine their post-buckling behavior. It is observed that the initial buckling is sensitive to initial geometrical imperfections but the post-buckling load is little influenced. Therefore, the post-buckling load is used to predict a more realistic load as compared to classical buckling theory prediction

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