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	<title><![CDATA[Scipedia: Papers Repository of the International Centre for Numerical Methods in Engineering (CIMNE)]]></title>
	<link>https://www.scipedia.com/sj/pr-cimne</link>
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	<guid isPermaLink="true">https://www.scipedia.com/public/Codina_Zienkiewicz_2001a</guid>
	<pubDate>Mon, 02 Sep 2019 15:43:30 +0200</pubDate>
	<link>https://www.scipedia.com/public/Codina_Zienkiewicz_2001a</link>
	<title><![CDATA[CBS versus GLS stabilization of the incompressible Navier–Stokes equations and the role of the time step as stabilization parameter]]></title>
	<description><![CDATA[<p><span style="color: rgb(28, 29, 30); font-size: 16px; font-style: normal; font-weight: 400;">In this work we compare two apparently different stabilization procedures for the finite element approximation of the incompressible Navier&ndash;Stokes equations. The first is the characteristic‐based split (CBS). It combines the characteristic Galerkin method to deal with convection dominated flows with a classical splitting technique, which in some cases allows us to use equal velocity&ndash;pressure interpolations. The second approach is the Galerkin‐least‐squares (GLS) method, in which a least‐squares form of the element residual is added to the basic Galerkin equations. It is shown that both formulations display similar stabilization mechanisms, provided the stabilization parameter of the GLS method is identified with the time step of the CBS approach. This identification can be understood from a formal Fourier analysis of the linearized problem.</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Codina_et_al_2001a</guid>
	<pubDate>Mon, 02 Sep 2019 15:32:20 +0200</pubDate>
	<link>https://www.scipedia.com/public/Codina_et_al_2001a</link>
	<title><![CDATA[Implementation of a stabilized finite element formulation for the incompressible Navier-Stokes equations based on a pressure gradient projection]]></title>
	<description><![CDATA[<p><span style="font-size: 12.8px; font-style: normal; font-weight: 400;">We discuss in this paper some implementation aspects of a finite element formulation for the incompressible Navier-Stokes which allows the use of equal order velocity-pressure interpolations. The method consists in introducing the project of the pressure gradient and adding the difference between the pressure Laplacian and divergence of this new field to the incompressibility equations, both multiplied by suitable algorithmic parameters. The main purpose of this paper is to discuss how to deal with the new variable in the implementation of the algorithm. Obviously, it could be treated as one extra unknown, either explicitly or as a condensed variable. However, we take for granted that the only way or another. Here we discuss some iterative schemes to perform this uncoupling of the pressure gradient projection (PGP) from the calculation of the velocity and the pressure, both for stationary and the transient of the linearization loop and the iterative segregation of the PGP, whereas in the second the main dilemma concerns the explicit or implicit treatment of the PGP.&nbsp;&nbsp;</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Folch_et_al_2001a</guid>
	<pubDate>Mon, 02 Sep 2019 15:26:38 +0200</pubDate>
	<link>https://www.scipedia.com/public/Folch_et_al_2001a</link>
	<title><![CDATA[Numerical modeling of magma withdrawal during explosive caldera-forming eruptions]]></title>
	<description><![CDATA[<p>We propose a simple physical model to characterize the dynamics of magma withdrawal during the course of caldera-forming eruptions. Simplification involves considering such eruptions as a piston-like system in which the host rock is assumed to subside as a coherent rigid solid. Magma behaves as a Newtonian incompressible fluid below the exsolution level and as a compressible gas-liquid mixture above this level. We consider caldera-forming eruptions within the frame of fluid-structure interaction problems, in which the flow-governing equations are written using an arbitrary Lagrangian-Eulerian (ALE) formulation. We propose a numerical procedure to solve the ALE governing equations in the context of a finite element method. The numerical methodology is based on a staggered algorithm in which the flow and the structural equations are alternatively integrated in time by using separate solvers. The procedure also involves the use of the quasi-Laplacian method to compute the ALE mesh of the fluid and a new conservative remeshing strategy. Despite the fact that we focus the application of the procedure toward modeling caldera-forming eruptions, the numerical procedure is of general applicability. The numerical results have important geological implications in terms of magma chamber dynamics during explosive caldera-forming eruptions. Simulations predict a nearly constant velocity of caldera subsidence that strongly depends on magma viscosity. They also reproduce the characteristic eruption rates of the different phases of an explosive calderaforming eruption. Numerical results indicate that the formation of vortices beneath the ring fault, which may allow mingling and mixing of parcels of magma initially located at different depths in the chamber, is likely to occur for low-viscosity magmas. Numerical results confirm that exsolution of volatiles is an efficient mechanism to sustain explosive caldera-forming eruptions and to explain the formation of large volumes of ignimbrites.</p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Blasco_Codina_2001a</guid>
	<pubDate>Mon, 02 Sep 2019 15:17:21 +0200</pubDate>
	<link>https://www.scipedia.com/public/Blasco_Codina_2001a</link>
	<title><![CDATA[Space and time error estimates for a first order, pressure stabilized finite element method for the incompressible Navier–Stokes equations]]></title>
	<description><![CDATA[<div id="abstracts" style="font-size: 18px; color: rgb(46, 46, 46); font-style: normal; font-weight: 400;"><div id="aep-abstract-id3" style="margin-bottom: 8px;"><div id="aep-abstract-sec-id4"><p style="margin-bottom: 16px;">In this paper we analyze a pressure stabilized, finite element method for the unsteady, incompressible Navier&ndash;Stokes equations in primitive variables; for the time discretization we focus on a fully implicit, monolithic scheme. We provide some error estimates for the fully discrete solution which show that the velocity is first order accurate in the time step and attains optimal order accuracy in the mesh size for the given spatial interpolation, both in the spaces&nbsp;<span><span id="MathJax-Element-1-Frame" style="font-style: normal; font-weight: normal; font-size: 16.2px; float: none;"><span>L2(&Omega;)</span></span></span>&nbsp;and&nbsp;<span><span id="MathJax-Element-2-Frame" style="font-style: normal; font-weight: normal; font-size: 16.2px; float: none;"><span>H10(&Omega;)</span></span></span>; the pressure solution is shown to be order&nbsp;<span><span id="MathJax-Element-3-Frame" style="font-style: normal; font-weight: normal; font-size: 16.2px; float: none;"><span>12</span></span></span>&nbsp;accurate in the time step and also optimal in the mesh size. These estimates are proved assuming only a weak compatibility condition on the approximating spaces of velocity and pressure, which is satisfied by equal order interpolations.</p></div></div></div>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Codina_2001b</guid>
	<pubDate>Mon, 02 Sep 2019 15:12:17 +0200</pubDate>
	<link>https://www.scipedia.com/public/Codina_2001b</link>
	<title><![CDATA[Pressure stability in fractional step finite element methods for incompressible flows]]></title>
	<description><![CDATA[<p><span style="font-size: 12.8px; font-style: normal; font-weight: 400;">The objective of this paper is to analyze the pressure stability of fractional step finite element methods for incompressible flows. For the classical first order projection method, it is shown that there is a pressure control which depends on the time step size, and therefore there is a lower bound for this time step for stability reasons. The situation is much worse for a second order scheme in which part of the extremely weak. To overcome these shortcomings, a stabilized fractional step finite element method is also considered, and its stability is analyzed. Some simple numerical examples are presented to support the theoretical results.</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Houzeaux_Codina_2001a</guid>
	<pubDate>Mon, 02 Sep 2019 14:35:32 +0200</pubDate>
	<link>https://www.scipedia.com/public/Houzeaux_Codina_2001a</link>
	<title><![CDATA[Transmission conditions with constraints in finite element domain decomposition methods for flow problems]]></title>
	<description><![CDATA[<p><span style="color: rgb(28, 29, 30); font-size: 16px; font-style: normal; font-weight: 400;">This work presents a conservative scheme for iteration‐by‐subdomain domain decomposition (DD) strategies applied to the finite element solution of flow problems. The DD algorithm is based on the iterative update of the boundary conditions on the interfaces between the subregions, the so‐called transmission conditions. The transmission conditions involve the essential and natural boundary conditions of the weak form of the problem, and should ensure strong continuity of the velocity and weak continuity of the traction. As a first approach, the transmission conditions are interpolated using the classical Lagrange interpolation functions. Conservation problems might arise when two adjacent subdomains have a sensibly different mesh spacing. In order to conserve any desired quantity of interest, an interface constraining is introduced: continuity of the transmission conditions are constrained under a scalar conservation equation. An example of mass conservation illustrates the algorithm.&nbsp;</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Codina_2001a</guid>
	<pubDate>Mon, 02 Sep 2019 14:25:30 +0200</pubDate>
	<link>https://www.scipedia.com/public/Codina_2001a</link>
	<title><![CDATA[A stabilized finite element method for generalized stationary incompressible flows]]></title>
	<description><![CDATA[<p><span style="font-size: 12.8px; font-style: normal; font-weight: 400;">In this paper we describe a finite element formulation for the numerical solution of the stationary Navier-Stokes equations including Coriolis forces and the permeability of the medium. The stabilized method is based on the algebraic version of the sub-grid scale approach. We first describe this technique for general systems of convection-diffusion-reaction equations and then we apply it to linearized flow equations. The important point is the design of the matrix of stabilization parameters that the method has. This design is based on the identification of the stability problems of the Galerkin method and a scaling of variables argument to determine which coefficients must be included in the stabilization matrix. This, together with the convergence analysis of the linearized problem, leads to a simple expression for the stabilization parameters in the general situation considered in the paper. The numerical analysis of the linearized problem also shows that the method has optimal convergence properties.&nbsp; &nbsp;&nbsp;</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Agelet_de_Saracibar_et_al_2001a</guid>
	<pubDate>Wed, 03 Apr 2019 11:24:22 +0200</pubDate>
	<link>https://www.scipedia.com/public/Agelet_de_Saracibar_et_al_2001a</link>
	<title><![CDATA[On the constitutive modeling of coupled thermomechanical phase-change problems]]></title>
	<description><![CDATA[<p><span style="color: rgb(46, 46, 46); font-size: 18px; font-style: normal; font-weight: 400;">This paper deals with a thermodynamically consistent numerical formulation for coupled thermoplastic problems including phase-change phenomena and frictional contact. The final goal is to get an accurate, efficient and robust numerical model, able for the numerical simulation of industrial solidification processes. Some of the current issues addressed in the paper are the following. A fractional step method arising from an operator split of the governing differential equations has been used to solve the nonlinear coupled system of equations, leading to a staggered product formula solution algorithm. Nonlinear stability issues are discussed and isentropic and isothermal operator splits are formulated. Within the isentropic split, a strong operator split design constraint is introduced, by requiring that the elastic and plastic entropy, as well as the phase-change induced elastic entropy due to the latent heat, remain fixed in the mechanical problem. The formulation of the model has been consistently derived within a thermodynamic framework. All the material properties have been considered to be temperature dependent. The constitutive behavior has been defined by a thermoviscous/elastoplastic free energy function, including a thermal multiphase change contribution. Plastic response has been modeled by a J2 temperature dependent model, including plastic hardening and thermal softening. The constitutive model proposed accounts for a continuous transition between the initial liquid state, the intermediate mushy state and the final solid state taking place in a solidification process. In particular, a pure viscous deviatoric model has been used at the initial fluid-like state. A thermomecanical contact model, including a frictional hardening and temperature dependent coupled potential, is derived within a fully consistent thermodinamical theory. The numerical model has been implemented into the computational finite element code COMET developed by the authors. Numerical simulations of solidification processes show the good performance of the computational model developed.</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Rojek_et_al_2001a</guid>
	<pubDate>Fri, 18 Jan 2019 12:21:24 +0100</pubDate>
	<link>https://www.scipedia.com/public/Rojek_et_al_2001a</link>
	<title><![CDATA[Advances in FE explicit formulation for simulation of metalforming processes]]></title>
	<description><![CDATA[<p style="margin-bottom: 16px; color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;">This paper presents some advances of finite element explicit formulation for simulation of metal forming processes. Because of their computational efficiency, finite element programs based on the explicit dynamic formulation proved to be a very attractive tool for the simulation of metal forming processes. The use of explicit programs in the sheet forming simulation is quite common, the possibilities of these codes in bulk forming simulation in our opinion are still not exploited sufficiently. In our paper, we will consider aspects of bulk forming simulation.</p><p style="margin-bottom: 16px; color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;">We will present new formulations and algorithms developed for bulk metal forming within the explicit formulation. An extension of a finite element code for the thermomechanical coupled analysis is discussed. A new thermomechanical constitutive model developed by the authors and implemented in the program is presented.</p><p style="margin-bottom: 16px; color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;">A new formulation based on the so-called split algorithm allows us to use linear triangular and tetrahedral elements in the analysis of large plastic deformations characteristic to forming processes. Linear triangles and tetrahedra have many advantages over quadrilateral and hexahedral elements. Linear triangles and tetrahedra based on the standard formulations exhibit volumetric locking and are not suitable for large plastic strain simulation. The new formulation allows to overcome this difficulty.</p><p style="margin-bottom: 16px; color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;">New formulations and algorithms have been implemented in the finite element code Stampack developed at the International Centre for Numerical Methods in Engineering in Barcelona. Numerical examples illustrate some of the possibilities of the finite element code developed and validate new algorithms.</p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Onate_et_al_2019a</guid>
	<pubDate>Fri, 04 Jan 2019 12:07:16 +0100</pubDate>
	<link>https://www.scipedia.com/public/Onate_et_al_2019a</link>
	<title><![CDATA[Combination of the critical displacement method with a damage model for structural instability analysis]]></title>
	<description><![CDATA[<p>The paper describes the extension of the critical<br />
displacement method (CDM), presented by O&ntilde;ate and Matias in 1996,<br />
to the instability analysis of structures with non-linear material<br />
behaviour using a simple damage model. The extended CDM is useful<br />
to detect instability points using a prediction of the critical<br />
displacement field and a secant load-displacement relationship<br />
accounting for material non-linearities. Examples of application<br />
of CDM to the instability analysis of structures using bar and<br />
solid finite elements are presented.</p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Scotta_et_al_2001a</guid>
	<pubDate>Mon, 07 Jan 2019 13:57:07 +0100</pubDate>
	<link>https://www.scipedia.com/public/Scotta_et_al_2001a</link>
	<title><![CDATA[A scalar damage model with a shear retention factor for the analysis of reinforced concrete structures: theory and validation]]></title>
	<description><![CDATA[<p><span style="color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;">A local&nbsp;isotropic<span>&nbsp;single parameter&nbsp;scalar&nbsp;model that can simulate the mechanical behaviour of quasi-brittle materials</span></span><span style="color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;"><span><span>, such as concrete, is described. The&nbsp;constitutive law<span><span>&nbsp;needs the mechanical characteristics and the&nbsp;fracture energy&nbsp;of concrete to be completely defined. The&nbsp;</span>damage parameter<span>&nbsp;is obtained directly from the value of an equivalent effective stress in order to reduce the computing effort. Due to the unique damage parameter, this model is suitable for the study of quasi-static problems involving monotonically increasing loads. The problem of&nbsp;localisation&nbsp;and mesh dependency have been partially overcome by using an enhanced local method in which a characteristic&nbsp;</span></span></span>internal length&nbsp;related to the mesh dimension is employed instead of the characteristic&nbsp;</span>fracture length<span><span>. In this work, the model was enriched further with the introduction of a shear&nbsp;retention factor<span>&nbsp;that accounts for the friction between the two surfaces of a crack. These new features assure a real improvement of the damage model, maintaining nevertheless its simplicity and low computing cost and making it suitable for the&nbsp;practical solution&nbsp;of&nbsp;</span></span>large scale problems<span><span>. Several&nbsp;numerical simulations&nbsp;of experimental tests, concerning fracture tests on&nbsp;</span>concrete specimens and beams&nbsp;failing in shear, have been performed for the validation of the model. The main results from the numerical analyses are described and compared with the experimental ones.</span></span></span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Onate_et_al_2001a</guid>
	<pubDate>Mon, 07 Jan 2019 13:45:56 +0100</pubDate>
	<link>https://www.scipedia.com/public/Onate_et_al_2001a</link>
	<title><![CDATA[A finite point method for elasticity problems]]></title>
	<description><![CDATA[<div><span style="color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;"><span>The basis of the finite&nbsp;point method&nbsp;(FPM) for the fully meshless solution of&nbsp;</span>elasticity problems&nbsp;in structural mechanics</span><span style="color: rgb(80, 80, 80); font-size: 16px; font-style: normal; font-weight: 400;"><span><span>&nbsp;is described. A stabilization technique based on a finite&nbsp;calculus&nbsp;procedure is used to improve the quality of the&nbsp;</span>numerical solution. The efficiency and accuracy of the stabilized FPM in the meshless analysis of simple linear elastic&nbsp;</span>structural problems&nbsp;is shown in some examples of applications.</span></div>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Onate_Zarate_2000b</guid>
	<pubDate>Wed, 12 Dec 2018 12:50:18 +0100</pubDate>
	<link>https://www.scipedia.com/public/Onate_Zarate_2000b</link>
	<title><![CDATA[Rotation‐free triangular plate and shell elements]]></title>
	<description><![CDATA[<p><span style="color: rgb(28, 29, 30); font-size: 16px; font-style: normal; font-weight: 400;">The paper describes how the finite element method and the finite volume method can be successfully combined to derive two new families of thin plate and shell triangles with translational degrees of freedom as the only nodal variables. The simplest elements of the two families based on combining a linear interpolation of displacements with cell centred and cell vertex finite volume schemes are presented in detail. Examples of the good performance of the new rotation‐free plate and shell triangles are given.</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Chiandussi_et_al_2018a</guid>
	<pubDate>Fri, 23 Nov 2018 14:27:28 +0100</pubDate>
	<link>https://www.scipedia.com/public/Chiandussi_et_al_2018a</link>
	<title><![CDATA[Shape variable definition with C0 , C1 and C2 continuity functions]]></title>
	<description><![CDATA[<p>The present paper proposes a new technique for the definition of the shape design variables in 2D and 3D optimisation problems. It can be applied to the discrete model of the analysed structure or to the original geometry without any previous knowledge of the analytical expression of the CAD defining surfaces. The proposed technique allows the surface continuity to be preserved during the geometry modification process to be defined a priori. This capability allows for the definition of shape variables suitable for every kind of discipline involved in the optimisation process (structural analysis, fluid-dynamic analysis, crash analysis, aerodynamic analysis, etc.).</p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Car_et_al_2018a</guid>
	<pubDate>Tue, 20 Nov 2018 13:32:06 +0100</pubDate>
	<link>https://www.scipedia.com/public/Car_et_al_2018a</link>
	<title><![CDATA[An anisotropic elastoplastic constitutive model for large deformation analysis of fibre reinforced composites]]></title>
	<description><![CDATA[<p>In this work a generalized anisotropic elastoplastic constitutive model in large deformation is presented. It is used for the analysis of fiber-reinforced composite materials in the frame of the finite element method. Mixing theory is applied to simulate the behavior of the composite material.&nbsp; The elastic anisotropic behavior&nbsp; is simulated with classical elasticity theory, while that of a non-proportional anisotropic solid is simulated by means of the proposed generalized anisotropic elastoplastic model. The&nbsp; approach assumes the existence of a real anisotropic space and of a fictitious isotropic space where a mapped fictitious problem is solved. Both spaces are related by means of a linear transformation using a fourth order&nbsp; tensor incorporating complete information on the real anisotropic material. Details of the numerical implementations of the model into a non-linear, large deformations finite element solution scheme are provided. Examples of application showing the performance of the model for the analysis of fiber-reinforced composite materials are given.</p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Onate_2000a</guid>
	<pubDate>Tue, 20 Nov 2018 13:22:17 +0100</pubDate>
	<link>https://www.scipedia.com/public/Onate_2000a</link>
	<title><![CDATA[A stabilized finite element method for incompressible viscous flows using a finite increment calculus formulation]]></title>
	<description><![CDATA[<p>A stabilized finite element formulation for incompressible viscous flows is derived. The starting point are the modified Navier-Stokes equations incorporating naturally the necessary stabilization terms via a finite increment calculus (FIC) procedure. Application of the standard finite element Galerkin method to the modified differential equations leads to a stabilized discrete system of equations overcoming the numerical instabilities emanating from the advective terms and those due to the lack of compatibility between approximate velocity and pressure fields. The FIC method also provides a natural explanation for the stabilization terms appearing in all equations for both the Navier-Stokes and the simpler Stokes equations. Transient solution schemes with enhanced stabilization properties are also proposed. Finally a procedure for computing the stabilization parameters is presented.</p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Draft_Samper_809758956</guid>
	<pubDate>Wed, 20 Nov 2019 11:44:53 +0100</pubDate>
	<link>https://www.scipedia.com/public/Draft_Samper_809758956</link>
	<title><![CDATA[Desarrollos y aplicaciones de modelos de fractura en la escuela de ingenieros de caminos de Barcelona]]></title>
	<description><![CDATA[<p>El art&iacute;culo es una panor&aacute;mica de los aspectos te&oacute;ricos y algunas aplicaciones pr&aacute;cticas de los modelos de fractura desarrollados por diversos grupos en la Escuela de Ingenieros de Caminos de Barcelona (EICB) durante los &uacute;ltimos quince a&ntilde;os para el an&aacute;lisis no lineal de estructuras. La motivaci&oacute;n fundamental para el desarrollo de estos modelos se centra en el an&aacute;lisis de la seguridad de estructuras de hormig&oacute;n en masa y armado. La mayor parte de los modelos se basan en la teor&iacute;a de da&ntilde;o continuo y utilizan el m&eacute;todo de los elementos finitos para la soluci&oacute;n num&eacute;rica. Los modelos de da&ntilde;o se han extendido y aplicado tambi&eacute;n con &eacute;xito al an&aacute;lisis de diversas estructuras de edificios hist&oacute;ricos. Los desarrollos m&aacute;s recientes de estos modelos en la EICB incluyen la predicci&oacute;n de fen&oacute;menos de localizaci&oacute;n en estructuras de hormig&oacute;n y el an&aacute;lisis del comportamiento no lineal de estructuras con materiales compuestos. De todos estos modelos se presentan en el art&iacute;culo unas breves pinceladas, las aplicaciones m&aacute;s relevantes y las referencias donde pueden encontrarse los detalles sobre cada caso.</p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Diez_et_al_2000a</guid>
	<pubDate>Thu, 24 Oct 2019 13:27:02 +0200</pubDate>
	<link>https://www.scipedia.com/public/Diez_et_al_2000a</link>
	<title><![CDATA[Adaptivity based on error estimation for viscoplastic softening materials]]></title>
	<description><![CDATA[<p><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">This paper focuses on the numerical simulation of strain softening mechanical problems. Two problems arise: (1) the constitutive model has to be regular and (2) the numerical technique must be able to capture the two scales of the problem (the macroscopic geometrical representation and the microscopic behavior in the localization bands). The Perzyna viscoplastic model is used in order to obtain a regularized softening model allowing to simulate strain localization phenomena.</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">This model is applied to quasistatic examples. The viscous regularization of quasistatic processes is also discussed: in quasistatics, the internal length associated with the obtained band width is no longer only a function of the material parameters but also depends on the boundary value problem (geometry and loads, specially loading velocity). An adaptive computation is applied to softening viscoplastic materials showing strain localization. As the key ingredient of the adaptive strategy, a residual type error estimator is generalized to deal with such highly nonlinear material model. In several numerical examples the adaptive process is able to detect complex collapse modes that are not captured by a first, even if fine, mesh. Consequently, adaptive strategies are found to be essential to detect the collapse mechanism and to assess the optimal location of the elements in the mesh.</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Huerta_Diez_2000a</guid>
	<pubDate>Thu, 24 Oct 2019 13:11:48 +0200</pubDate>
	<link>https://www.scipedia.com/public/Huerta_Diez_2000a</link>
	<title><![CDATA[Error estimation including pollution assessment for nonlinear finite element analysis]]></title>
	<description><![CDATA[<p><span style="color: rgb(46, 46, 46); font-size: 18px; font-style: normal; font-weight: 400;">A residual type error estimator for nonlinear finite element analysis is introduced. This error estimator solves local problems avoiding both the computation of the flux jumps and the associated flux splitting procedure. Pollution errors are taken into account by a feedback strategy, that is, an error estimate based on local computations is used as the input of the pollution analysis. This estimator is used in the frame of an adaptive procedure. Numerical examples show that the estimator is able to drive adaptive procedures leading to likely good solutions. Moreover, one of the examples demonstrates that adaptive procedures are essential for complex highly nonlinear mechanical problems because they may discover secondary collapse mechanisms.</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
<item>
	<guid isPermaLink="true">https://www.scipedia.com/public/Diez_Huerta_2000a</guid>
	<pubDate>Thu, 24 Oct 2019 11:33:01 +0200</pubDate>
	<link>https://www.scipedia.com/public/Diez_Huerta_2000a</link>
	<title><![CDATA[Error estimation for adaptive computations on shell structures]]></title>
	<description><![CDATA[<p><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">The finite element discretization of a shell structure introduces two kinds of</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">errors: the error in the functional approximation and the error in the geometry</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">approximation. The first is associated with the finite dimensional interpolation</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">space and it is present in any finite element computation. The latter is associated</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">with the piecewise polynomial approximation of a curved surface and is much more</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">relevant in shell problems than in any other standard 2D or 3D computation. In</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">the shells framework, formerly the quality control of the finite element solution</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">has been carried out using flux projection a posteriori error estimators. This</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">technique exhibits two main drawbacks: 1) the flux smoothing averages stress components</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">over different elements that may have different physical meaning if the tangent</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">planes are different and 2) the error estimation process uses only the approximate</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">solution and hence, the discretized forces and the computational mesh: the data</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">describing the real geometry and load is therefore not accounted for. In this</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">work, a residual type error estimator introduced for standard 2D finite element</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">analysis is generalized to shell problems. This allows to easily account for the</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">real original geometry of the problem in the error estimation procedure and precludes</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">the necessity of comparing generalized stress components between non coplanar</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">elements. This estimator is based on approximating a reference error associated</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">with a refined reference mesh. In order to build up the residual error equation</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">the computed solution must be represented (projected) on the reference mesh. The</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">use of thin shell finite elements requires a proper formulation in order to preclude</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">shear locking. Following an idea of Donea and Lamain, the interpolation of the</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">rotations is not unique and requires a particular technique to transfer the information</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">from the computational mesh to the reference mesh. This technique is also developed</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">in this work and may be used in any adaptive evolution problem where the solution</span><br style="color: rgb(116, 116, 116); font-size: 18px;"><span style="color: rgb(116, 116, 116); font-size: 18px; font-style: normal; font-weight: 400;">must be transferred from one mesh to another.</span></p>]]></description>
	<dc:creator>María Jesús Samper</dc:creator>
</item>
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