The thesis presents a novel computational method for analysing the static and dynamic behaviour of a multi-damaged beam using local and non-local elasticity theories. Most of the lumped damage beam models proposed to date are based on slender beam theory in classical (local) elasticity and are limited by inaccuracies caused by the implicit assumption of the Euler-Bernoulli beam model and by the spring model itself, which simplifies the real beam behaviour around the crack. In addition, size effects and material heterogeneity cannot be taken into account using the classical elasticity theory due to the absence of any microstructural parameter. The proposed work is based on the inhomogeneous Euler-Bernoulli beam theory in which a Dirac's delta function is added to the bending flexibility at the position of each crack: that is, the severer the damage, the larger is the resulting impulsive term. The crack is assumed to be always open, resulting in a linear system (i.e. nonlinear phenomena associated with breathing cracks are not considered). In order to provide an accurate representation of the structure's behaviour, a new multi-cracked beam element including shear effects and rotatory inertia is developed using the flexibility approach for the concentrated damage. The resulting stiffness matrix and load vector terms are evaluated by the unit-displacement method, employing the closed-form solutions for the multi-cracked beam problem. The same deformed shapes are used to derive the consistent mass matrix, also including the rotatory inertia terms. The two-node multi-damaged beam model has been validated through comparison of the results of static and dynamic analyses for two numerical examples against those provided by a commercial finite element code. The proposed model is shown to improve the computational efficiency as well as the accuracy, thanks to the inclusion of both shear deformations and rotatory inertia. The inaccuracy of the spring model, where for example for a rotational spring a finite jump appears on the rotations' profile, has been tackled by the enrichment of the elastic constitutive law with higher order stress and strain gradients. In particular, a new phenomenological approach based upon a convenient form of non-local elasticity beam theory has been presented. This hybrid non-local beam model is able to take into account the distortion on the stress/strain field around the crack as well as to include the microstructure of the material, without introducing any additional crack related parameters. The Laplace's transform method applied to the differential equation of the problem allowed deriving the static closed-form solution for the multi-cracked Euler-Bernoulli beams with hybrid non-local elasticity. The dynamic analysis has been performed using a new computational meshless method, where the equation of motions are discretised by a Galerkin-type approximation, with convenient shape functions able to ensure the same grade of approximation as the beam element for the classical elasticity. The importance of the inclusion of microstructural parameters is addressed and their effects are quantified also in comparison with those obtained using the classical elasticity theory.

This thesis presents an approach to modelling dynamic mass capture which is applied to a number of system models. The models range from a simple 2D Euler-Bernoulli beam with point masses for the end-effector and target to a 3D Timoshenko beam model (including torsion) with rigid bodies for the end-effector and target. In addition, new models for torsion, as well as software to derive the finite element equations from first principles were developed to support the modelling. Results of the models are compared to a simple experiment as done by Ben Rhody. Investigations of offset capture are done by simulation to show why one would consider using a 3D model that includes torsion. These problems have relevance to both terrestrial robots and to space based robotic systems such as the manipulators on the International Space Station capturing payloads such as the SpaceX Dragon capsule. One could increase production in an industrial environment if industrial robots could pick up items without having to establish a zero relative velocity between the end effector and the item. To have a robot acquire its payload in this way would introduce system dynamics that could lead to the necessity of modelling a previously ‘rigid’ robot as flexible.

This thesis is about using structural-dynamics based methods to address the existing challenges in the field of Structural Health Monitoring (SHM). Particularly, new structural-dynamics based methods are presented, to model areas of damage, to do damage diagnosis and to estimate and predict the sensitivity of structural vibration properties like natural frequencies to the presence of damage. Towards these objectives, a general analytical procedure, which yields nth-order expressions governing mode shapes and natural frequencies and for damaged elastic structures such as rods, beams, plates and shells of any shape is presented. Features of the procedure include the following: 1. Rather than modeling the damage as a fictitious elastic element or localized or global change in constitutive properties, it is modeled in a mathematically rigorous manner as a geometric discontinuity. 2. The inertia effect (kinetic energy), which, unlike the stiffness effect (strain energy), of the damage has been neglected by researchers, is included in it. 3. The framework is generic and is applicable to wide variety of engineering structures of different shapes with arbitrary boundary conditions which constitute self adjoint systems and also to a wide variety of damage profiles and even multiple areas of damage. To illustrate the ability of the procedure to effectively model the damage, it is applied to beams using Euler-Bernoulli and Timoshenko theories and to plates using Kirchhoff's theory, supported on different types of boundary conditions. Analytical results are compared with experiments using piezoelectric actuators and non-contact Laser-Doppler Vibrometer sensors. Next, the step of damage diagnosis is approached. Damage diagnosis is done using two methodologies. One, the modes and natural frequencies that are determined are used to formulate analytical expressions for a strain energy based damage index. Two, a new damage detection parameter are identified. Assuming the damaged structure to be a linear system, the response is expressed as the summation of the responses of the corresponding undamaged structure and the response (negative response) of the damage alone. If the second part of the response is isolated, it forms what can be regarded as the damage signature. The damage signature gives a clear indication of the damage. In this thesis, the existence of the damage signature is investigated when the damaged structure is excited at one of its natural frequencies and therefore it is called ``partial mode contribution". The second damage detection method is based on this new physical parameter as determined using the partial mode contribution. The physical reasoning is verified analytically, thereupon it is verified using finite element models and experiments. The limits of damage size that can be determined using the method are also investigated. There is no requirement of having a baseline data with this damage detection method. Since the partial mode contribution is a local parameter, it is thus very sensitive to the presence of damage. The parameter is also shown to be not affected by noise in the detection ambience.

This thesis presents an approach to modelling dynamic mass capture which is applied to a number of system models. The models range from a simple 2D Euler-Bernoulli beam with point masses for the end-effector and target to a 3D Timoshenko beam model (including torsion) with rigid bodies for the end-effector and target. In addition, new models for torsion, as well as software to derive the finite element equations from first principles were developed to support the modelling. Results of the models are compared to a simple experiment as done by Ben Rhody. Investigations of offset capture are done by simulation to show why one would consider using a 3D model that includes torsion. These problems have relevance to both terrestrial robots and to space based robotic systems such as the manipulators on the International Space Station capturing payloads such as the SpaceX Dragon capsule. One could increase production in an industrial environment if industrial robots could pick up items without having to establish a zero relative velocity between the end effector and the item. To have a robot acquire its payload in this way would introduce system dynamics that could lead to the necessity of modelling a previously ‘rigid’ robot as flexible.

Nonlinear finite element models of functionally graded beams with power-law variation of material, accounting for the von-Karman geometric nonlinearity and temperature dependent material properties as well as microstructure dependent length scale have been developed using the Euler-Bernoulli as well as the first-order and third- order beam theories. To capture the size effect, a modified couple stress theory with one length scale parameter is used. Such theories play crucial role in predicting accurate deflections of micro- and nano-beam structures. A general third order beam theory for microstructure dependent beam has been developed for functionally graded beams for the first time using a modified couple stress theory with the von Karman nonlinear strain. Finite element models of the three beam theories have been developed. The thermo-mechanical coupling as well as the bending-stretching coupling play significant role in the deflection response. Numerical results are presented to show the effect of nonlinearity, power-law index, microstructural length scale, and boundary conditions on the bending response of beams under thermo-mechanical loads. In general, the effect of microstructural parameter is to stiffen the beam, while shear deformation has the effect of modeling more realistically as a flexible beam.

A partial differential equation in space and time represents the physics of rotating beams. Mostly, the numerical solution of such an equation is an available option as analytical solutions are not feasible even for a uniform rotating beam. Although the numerical solutions can be obtained with a number of combinations (in space and time), one tries to seek for a better alternative. In this work, various numerical techniques are applied to the rotating beam problems: finite element method, meshless methods, and B-spline finite element methods. These methods are applied to the governing differential equations of a rotating Euler-Bernoulli beam, rotating Timoshenko beam, rotating Rayleigh beam, and cracked Euler-Bernoulli beam. This work provides some elegant alternatives to the solutions available in the literature, which are more efficient than the existing methods: the p-version of finite element in time for obtaining the time response of periodic ordinary differential equations governing helicopter rotor blade dynamics, the symmetric matrix formulation for a rotating Euler-Bernoulli beam free vibration problem using the Galerkin method, and solution for the Timoshenko beam governing differential equation for free vibration using the meshless methods. Also, the cracked Euler-Bernoulli beam free vibration problem is solved where the importance of higher order polynomial approximation is shown. Finally, the overall response of rotating blades subjected to aerodynamic forcing is obtained in uncoupled trim where the response is independent of the overall helicopter configuration. Stability analysis for the rotor blade in hover and forward flight is also performed using Floquet theory for periodic differential equations.

Sandwich constructions are the most commonly used structures in aircraft and navy industries, traditionally. These structures are made up of the face sheets and the core, where the face sheets will be taking the load and is connected to other structural members, while the soft core material, will be used to absorb energy during impact like situation. Thus, sandwich constructions are mainly employed in light weight structures where the high energy absorption capability is required. Generally the face sheets will be thin, made up of either metallic or composite material with high stiffness and strength, while the core is light in weight, made up of soft material. Cores generally play very crucial role in achieving the desired properties of sandwich structures, either through geometric arrangement or material properties or both. Foams are in extensive use nowadays as core material due to the ease in manufacturing and their low cost. They are extensively used in automotive and industrial field applications as the desired foam density can be fabricated by adjusting the mixing, curing and heat sink processes. Modeling of sandwich beams play a crucial role in their design with suitable finite elements for face sheets and core, to ensure the compatibility between degrees of freedom at the interfaces. Unless the mathematical model simulates the physics of the model in terms of kinematics, boundary and loading conditions, results predicted will not be accurate. Accurate models helps in obtaining an efficient design of sandwich beams. In Structural Health Monitoring studies, the responses under the impact loading will be captured by carrying out the wave propagation analysis. The loads applied will be for a shorter duration (in the orders of micro seconds), where higher frequency modes will be excited. Wavelengths at such high frequencies are very small and hence, in such cases, very fine mesh generally is employed matching the wavelength requirement of the propagating wave. Traditional Finite element softwares takes enormous time and computational e ort to provide the solution. Various possible models and modeling aspects using the existing Finite element tools for wave propagation analysis are studied in the present work. There exists a huge demand for an accurate, efficient and rapidly convergent finite elements for the analysis of sandwich beams. E orts are made in the present work to address these issues and provide a solution to the sandwich user community. Super convergent and Spectral Finite sandwich Beam Elements with metallic or composite face sheets and soft core are developed. As a philosophy, the sandwich beam finite element is constructed with the combination of two beams representing the face sheets (top and bottom) at their neutral axis. The core effects are captured at the interface boundaries in terms of shear stress and normal transverse stress. In the case of wave propagation analysis, the equations are coupled in time domain and spatial domain and solving them directly is a difficult task. In Spectral Finite Element Method(SFEM), the displacement functions are derived by solving the transformed governing equations in the frequency domain. By transforming them and forces from time domain to frequency domain, the coupled partial differential equations will become coupled ordinary differential equations. These equations in frequency domain, can be solved exactly as they are normally ordinary differential equation with constant coefficients with frequency entering as a parameter. These solutions will be used as interpolating functions for spectral element formulation and in this respect it differs from conventional FE method wherein mostly polynomials are used as interpolating functions. In addition, SFEM solutions are expressed in terms of forward and backward moving waves for all the degrees of freedom involved in the formulations and hence, SFEM provides faster and efficient solutions for wave propagation analysis. In the present work, strong form of the governing differential equations are derived for a given system using Hamilton's principle. Super Convergent elements are developed by solving the static part of the governing differential equations exactly and hence the stiffness matrix derived is exact for point static loads. For wave propagation analysis, as the mass is not exactly represented, these elements are required in the optimal numbers for getting good results. The number of these elements required are generally much lesser than the number of elements required using traditional finite elements since the stiffness distribution is exact. Spectral elements are developed by solving the governing equations exactly in the frequency domain and hence the dynamic stiffness matrix derived is exact for the dynamic loads. Hence, one element between any two joints is enough to solve the whole system under impact loads for simple structures. Developing FE for sandwich beams is quiet challenging. Due to small thickness, the face sheets can be modeled using 1D idealization, while modeling of large core requires 2-D idealization. Hence, most finite or spectral elements requires stitching of these two idealizations into 1-D idealization, which can be accomplished in a variety of ways, some of which are highlighted in this thesis. Variety of finite and spectral finite elements are developed considering Euler and Timoshenko beam theories for modeling the sandwich beams. Simple element models are built with rigid core in both the theories. Models are also developed considering the flexible core with the variation of transverse displacements across depth of the core. This has direct influence on shear stress variation and also transverse normal stress in the core. Simple to higher order models are developed considering different variations in shear stress and transverse normal stress across depth of the core. Development of super convergent finite Euler Bernoulli beam elements Eul4d (4 dof element), Eul10d (10 dof element) are explained along with their results in Chapter 2. Development of different super convergent finite Timoshenko beam elements namely Tim4d (4 dof), Tim7d (7 dof), Tim10d (10 dof) are explained in Chapter 3. Validation of Euler Bernoulli and Timoshenko elements developed in the present work is carried out with test cases available in the open literature for displacements and free vibration frequencies are presented in Chapter 2 and Chapter 3. The results indicates that all developed elements are performing exceedingly well for static loads and free vibration. Super convergence performance for the elements developed is demonstrated with related examples. Spectral elements based on Timoshenko theory STim7d, STim6d, STim6dF are developed and the wave propagation characteristics studies are presented in Chapter 4. Euler spectral elements are derived from Timoshenko spectral elements by enforcing in finite shear rigidity, designated as SEul7d, SEul6d, SEul6dF and are presented. E orts were made in this present work to model the horizontal cracks in top or bottom face sheets using the spectral elements and the methodology is presented in Chapter 4. Wave propagation analysis using general purpose software N AST RAN and the super convergent as well as spectral elements developed in this work, are discussed in detail in Chapter 5. Modeling aspects of sandwich beam in N AST RAN using various combination of elements available and the performance of four possible models simulated were studied. Validation of all four models in N AST RAN, Super convergent Euler, Timoshenko and Spectral Timoshenko finite elements was carried out by simulating a homogenous I beam by comparing the longitudinal and transverse responses. Studies were carried out to find out the response predictions of a sandwich beam with soft core and all the predictions were compared and discussed. The responses in case of cracks in top or bottom face sheets under the longitudinal and transverse loading were studied in this chapter. In Chapter 6, Parametric studies were carried out for bringing out the sensitiveness of the important specific parameters in overall behaviour and performance of a sandwich beam, using Super convergent and Spectral elements developed. This chapter clearly brings out the various aspects of design of sandwich beam such as material selection of core, geometrical configuration of overall beam and core. Effects of shear modulus, mass density on wave propagation characteristics, effects of thick or thin cores with reference to the face sheets and dynamic effects of core are highlighted. Wave propagation characteristics studies includes the study of wave numbers, group speeds, cut off frequencies for a given configuration and identification of frequency zone of operations. The recommendations for improvement in design of sandwich beams based on the parametric studies are made at the end of chapter. The entire thesis, written in seven Chapters, presents a unified treatment of sandwich beam analysis that will be very useful for designers working in the area.

Esta investigación se enfoca en el análisis de vibración libre de vigas Timoshenko utilizando el método de elementos finitos. Se desarrolla el modelo utilizando el principio de Hamilton y la teoría de vigas Timoshenko que incluye deformaciones por corte. Se asume interpolaciones de alto orden para la aproximación de las variables fundamentales. Los materiales para emplear son isotrópicos. Se implementa un programa para estos materiales en MATLAB. Se comparan resultados con otros obtenidos en la literatura para validar el modelo. Se realiza un estudio paramétrico con una misma longitud y diferentes esbelteces. Se verifica que la formulación sea bastante precisa con resultados muy satisfactorios. / This research focuses on the free vibration analysis of Timoshkenko beams using the finite element method. The model is developed using the Hamilton principle and the Timoshenko beam theory that includes shear deformations. high order interpolations are assumed for the approximation of the fundamental variables. The materials to be used are isotropic. A program for these materials is implemented in MATLAB. Results are compared with others obtained in the literature to validate the model. A parametric study is carried out with the same length and different slenderness. It is verified that the formulation is quite precise with satisfactory results to the investigation. / Trabajo de investigación

[pt] Uma análise não linear geométrica de estruturas, utilizando o Método dos Elementos Finitos (MEF), depende de cinco aspectos: a teoria de flexão, da descrição cinemática, das relações entre deformações e deslocamentos, da metodologia de análise não linear e das funções de interpolação de deslocamentos. Como o MEF é uma solução numérica, a discretização da estrutura fornece grande influência na resposta dessa análise. Contudo, ao se empregar funções de interpolação correspondentes à solução homogênea da equação diferencial do problema, obtêm-se o comportamento exato da estrutura para uma discretização mínima, como ocorre em uma análise linear. Assim, este trabalho visa a integrar as soluções para o problema da não linearidade geométrica, de maneira a tentar reduzir essa influência e permitir uma discretização mínima da estrutura, considerando ainda grandes deslocamentos e rotações. Então, utilizando-se a formulação Lagrangeana atualizada, os termos de ordem elevada no tensor deformação, as teorias de flexão de Euler-Bernoulli e Timoshenko, os algoritmos para solução de problemas não lineares e funções de interpolação, que consideram a influência da carga axial, obtidas da solução da equação diferencial do equilíbrio de um elemento infinitesimal na condição deformada, desenvolve-se um elemento de pórtico espacial com uma formulação completa. O elemento é implementado no Framoop e sua resposta, utilizando-se uma discretização mínima da estrutura, é comparada com formulações usuais, soluções analíticas e com o programa Mastan2 v3.5. Os resultados evidenciam a eficiência da formulação desenvolvida para prever a carga crítica de estruturas planas e espaciais utilizando uma discretização mínima. / [en] A structural geometric nonlinear analysis, using the finite element method (FEM), depends on the consideration of five aspects: the bending theory, the kinematic description, the strain-displacement relations, the nonlinear solution scheme and the interpolation (shape) functions. As MEF is a numerical solution, the structure discretization provides great influence on the analysis response. However, applying shape functions calculated from the homogenous solution of the differential equation of the problem, the exact behavior of the structure is obtained for a minimum discretization, as for a linear analysis. Thus, this work aims to integrate the solutions for the formulations of the geometric nonlinearity problem, in order to reduce this influence and allow a minimum discretization of the structure, also considering, large displacements and rotations. Then, using an updated Lagrangian kinematic description, considering a higher-order Green strain tensor, The Euler-Bernoulli and Timoshenko beam theories, the nonlinear solutions schemes and the interpolation functions, that includes the influence of axial force, obtained directly from the solution of the equilibrium differential equation of an deformed infinitesimal element, a spatial bar frame element is developed using a complete formulation. The element was implemented in the Framoop, and their results, for a minimum discretization, were compared with conventional formulations, analytical solutions and with the software Mastan2 v3.5. Results clearly show the efficiency of the developed formulation to predict the critical load of plane and spatial structures using a minimum discretization.

Dans ce travail, différentes formulations d'éléments de poutres sont proposées pour l'analyse à rupture de structures de type poutres ou portiques en béton armé soumises à des chargements statiques monotones. La rupture localisée des matériaux est modélisée par la méthode à discontinuité forte, qui consiste à enrichir l'interpolation standard des déplacements (ou rotations) avec des fonctions discontinues associées à un paramètre cinématique supplémentaire interprété comme un saut de déplacement (ou rotation). Ces paramètres additionnels sont locaux et condensés au niveau élémentaire. Un élément fini écrit en efforts résultants et deux éléments finis multi-couches sont développés dans ce travail. L'élément de poutre d'Euler Bernouilli écrit en effort résultant présente une discontinuité en rotation. La réponse en flexion du matériau hors discontinuité est décrite par un modèle élastoplastique en effort résultant et la relation cohésive liant moment et saut de rotation sur la rotule plastique est, quant à elle, décrite par un modèle rigide plastique. La réponse axiale est suppposée élastique. Pour ce qui concerne l'approche multi-couche, chaque couche est considérée comme une barre constituée de béton ou d'acier. La partie régulière de la déformation de chaque couche est calculée en s'appuyant sur la cinématique associée à la théorie d'Euler Bernoulli ou de Timoshenko. Une déformation axiale additionnelle est considérée par l'introduction d'une discontinuité du déplacement axial, introduite indépendamment dans chaque couche. Le comportement du béton est pris en compte par un modèle élasto-endommageable alors que celui de l'acier est décrit par un modèle élastoplastique. La relation cohésive entre la traction sur la discontinuité et le saut de déplacement axial est décrit par un modèle rigide endommageable adoucissant pour les barres (couches) en béton et rigide plastique adoucissant pour les barres en acier. La réponse en cisaillement pour l'élement de Timoshenko est supposée élastique. Enfin, l'élément multi-couche de Timoshenko est enrichi en introduisant une partie visqueuse dans la réponse adoucissante. L'implantation numérique des différents éléments développés dans ce travail est présentée en détail. La résolution par une procédure d'«operator split» est décrite pour chaque type d'élément. Les différentes quantités nécessaires pour le calcul au niveau local des variables internes des modèles non linéaires ainsi que pour la construction du système global fournissant les valeurs des dégrés de liberté sont précisées. Les performances des éléments développés sont illustrées à travers des exemples numériques montrant que la formulation basée sur un élément multicouche d'Euler Bernouilli n'est pas robuste alors les simulations s'appuyant sur des éléments d'Euler Bernouilli en efforts résultants ou sur des éléments multicouche de Timoshenko fournissent des résultats très satisfaisants. / In this work, several beam finite element formulations are proposed for failure analysis of planar reinforced concrete beams and frames under monotonic static loading. The localized failure of material is modeled by the embedded strong discontinuity concept, which enhances standard interpolation of displacement (or rotation) with a discontinuous function, associated with an additional kinematic parameter representing jump in displacement (or rotation). The new parameters are local and are condensed on the element level. One stress resultant and two multi-layer beam finite elements are derived. The stress resultant Euler-Bernoulli beam element has embedded discontinuity in rotation. Bending response of the bulk of the element is described by elasto-plastic stress resultant material model. The cohesive relation between the moment and the rotational jump at the softening hinge is described by rigid-plastic model. Axial response is elastic. In the multi-layer beam finite elements, each layer is treated as a bar, made of either concrete or steel. Regular axial strain in a layer is computed according to Euler-Bernoulli or Timoshenko beam theory. Additional axial strain is produced by embedded discontinuity in axial displacement, introduced individually in each layer. Behavior of concrete bars is described by elastodamage model, while elasto-plasticity model is used for steel bars. The cohesive relation between the stress at the discontinuity and the axial displacement jump is described by rigid-damage softening model in concrete bars and by rigid-plastic softening model in steel bars. Shear response in the Timoshenko element is elastic. Finally, the multi-layer Timoshenko beam finite element is upgraded by including viscosity in the softening model. Computer code implementation is presented in detail for the derived elements. An operator split computational procedure is presented for each formulation. The expressions, required for the local computation of inelastic internal variables and for the global computation of the degrees of freedom, are provided. Performance of the derived elements is illustrated on a set of numerical examples, which show that the multi-layer Euler-Bernoulli beam finite element is not reliable, while the stress-resultant Euler-Bernoulli beam and the multi-layer Timoshenko beam finite elements deliver satisfying results. / V disertaciji predlagamo nekaj formulacij končnih elementov za porušno analizo armiranobetonskih nosilcev in okvirjev pod monotono statično obteˇzbo. Lokalizirano porušitev materiala modeliramo z metodo vgrajene nezveznosti, pri kateri standardno interpolacijo pomikov (ali zasukov) nadgradimo z nezvezno interpolacijsko funkcijo in z dodatnim kinematičnim parametrom, ki predstavlja velikost nezveznosti v pomikih (ali zasukih). Dodatni parametri so lokalnega značaja in jih kondenziramo na nivoju elementa. Izpeljemo en rezultantni in dva večslojna končna elementa za nosilec. Rezultantni element za Euler-Bernoullijev nosilec ima vgrajeno nezveznost v zasukih. Njegov upogibni odziv opišemo z elasto-plastičnim rezultantnim materialnim modelom. Kohezivni zakon, ki povezuje moment v plastičnem členku s skokom v zasuku, opišemo s togo-plastičnim modelom mehčanja. Osni odziv je elastičen. V večslojnih končnih elementih vsak sloj obravnavamo kot betonsko ali jekleno palico. Standardno osno deformacijo v palici izračunamo v skladu z Euler-Bernoullijevo ali s Timošenkovo teorijo nosilcev. Vgrajena nezveznost v osnem pomiku povzroči dodatno osno deformacijo v posamezni palici. Obnašanje betonskega sloja opišemo z modelom elasto-poškodovanosti, za sloj armature pa uporabimo elasto-plastični model. Kohezivni zakon, ki povezuje napetost v nezveznosti s skokom v osnem pomiku, opišemo z modelom mehčanja v poškodovanosti za beton in s plastičnim modelom mehčanja za jeklo.Striˇzni odziv Timošenkovega nosilca je elastičen. Večslojni končni element za Timošenkov nosilec nadgradimo z viskoznim modelom mehčanja. Za vsak končni element predstavimo računski algoritem ter vse potrebne izraze za lokalni izračun neelastičnih notranjih spremenljivk in za globalni izračun prostostnih stopenj. Delovanje končnih elementov preizkusimo na več numeričnih primerih. Ugotovimo, da večslojni končni element za Euler-Bernoullijev nosilec ni zanesljiv, medtem ko rezultantni končni element za Euler-Bernoullijev nosilec in večslojni končni element za Timošenkov nosilec dajeta zadovoljive rezultate.