An improved finite element space for discontinuous pressures

We consider incompressible Stokes flow with an internal interface at which the pressure is discontinuous, as happens for example in problems involving surface tension. We assume that the mesh does not follow the interface, which makes classical interpolation spaces to yield suboptimal convergence rates (typically, the interpolation error in the L(2)(Omega)-norm is of order h(1/2)). We propose a modification of the P(1)-conforming space that accommodates discontinuities at the interface without introducing additional degrees of freedom or modifying the sparsity pattern of the linear system. The unknowns are the pressure values at the vertices of the mesh and the basis functions are computed locally at each element, so that the implementation of the proposed space into existing codes is straightforward. With this modification, numerical tests show that the interpolation order improves to O(h(3/2)). The new pressure space is implemented for the stable P(1)(+)/P(1) mini-element discretization, and for the stabilized equal-order P(1)/P(1) discretization. Assessment is carried out for Poiseuille flow with a forcing surface and for a static bubble. In all cases the proposed pressure space leads to improved convergence orders and to more accurate results than the standard P(1) space. In addition, two Navier-Stokes simulations with moving interfaces (Rayleigh-Taylor instability and merging bubbles) are reported to show that the proposed space is robust enough to carry out realistic simulations. (c) 2009 Elsevier B.V. All rights reserved.

Evaluation of a bounded high order upwind scheme for 3D incompressible free surface flow computations

fit the context of normalized variable formulation (NVF) of Leonard and total variation diminishing (TVD) constraints of Harten. this paper presents an extension of it previous work by the authors for solving unsteady incompressible flow problems. The main contributions of the paper are threefold. First, it presents the results of the development and implementation of a bounded high order upwind adaptative QUICKEST scheme in the 3D robust code (Freeflow), for the numerical solution of the full incompressible Navier-Stokes equations. Second, it reports numerical simulation results for 1D hock tube problem, 2D impinging jet and 2D/3D broken clam flows. Furthermore, these results are compared with existing analytical and experimental data. And third, it presents the application of the numerical method for solving 3D free surface flow problems. (C) 2007 IMACS. Published by Elsevier B.V. All rights reserved,

Stability of numerical schemes on staggered grids

This paper considers the stability of explicit, implicit and Crank-Nicolson schemes for the one-dimensional heat equation on a staggered grid. Furthemore, we consider the cases when both explicit and implicit approximations of the boundary conditions arc employed. Why we choose to do this is clearly motivated and arises front solving fluid flow equations with free surfaces when the Reynolds number can be very small. in at least parts of the spatial domain. A comprehensive stability analysis is supplied: a novel result is the precise stability restriction on the Crank-Nicolson method when the boundary conditions are approximated explicitly, that is, at t =n delta t rather than t = (n + 1)delta t. The two-dimensional Navier-Stokes equations were then solved by a marker and cell approach for two simple problems that had analytic solutions. It was found that the stability results provided in this paper were qualitatively very similar. thereby providing insight as to why a Crank-Nicolson approximation of the momentum equations is only conditionally, stable. Copyright (C) 2008 John Wiley & Sons, Ltd.

A discontinuous-Galerkin-based immersed boundary method

A numerical method to approximate partial differential equations on meshes that do not conform to the domain boundaries is introduced. The proposed method is conceptually simple and free of user-defined parameters. Starting with a conforming finite element mesh, the key ingredient is to switch those elements intersected by the Dirichlet boundary to a discontinuous-Galerkin approximation and impose the Dirichlet boundary conditions strongly. By virtue of relaxing the continuity constraint at those elements. boundary locking is avoided and optimal-order convergence is achieved. This is shown through numerical experiments in reaction-diffusion problems. Copyright (c) 2008 John Wiley & Sons, Ltd.

An implicit technique for solving 3D low Reynolds number moving free surface flows

This paper describes the development of an implicit finite difference method for solving transient three-dimensional incompressible free surface flows. To reduce the CPU time of explicit low-Reynolds number calculations, we have combined a projection method with an implicit technique for treating the pressure on the free surface. The projection method is employed to uncouple the velocity and the pressure fields, allowing each variable to be solved separately. We employ the normal stress condition on the free surface to derive an implicit technique for calculating the pressure at the free surface. Numerical results demonstrate that this modification is essential for the construction of methods that are more stable than those provided by discretizing the free surface explicitly. In addition, we show that the proposed method can be applied to viscoelastic fluids. Numerical results include the simulation of jet buckling and extrudate swell for Reynolds numbers in the range [0.01, 0.5]. (C) 2008 Elsevier Inc. All rights reserved.

Numerical Solution of the Upper-Convected Maxwell Model for Three-Dimensional Free Surface Flows

This work presents a finite difference technique for simulating three-dimensional free surface flows governed by the Upper-Convected Maxwell (UCM) constitutive equation. A Marker-and-Cell approach is employed to represent the fluid free surface and formulations for calculating the non-Newtonian stress tensor on solid boundaries are developed. The complete free surface stress conditions are employed. The momentum equation is solved by an implicit technique while the UCM constitutive equation is integrated by the explicit Euler method. The resulting equations are solved by the finite difference method on a 3D-staggered grid. By using an exact solution for fully developed flow inside a pipe, validation and convergence results are provided. Numerical results include the simulation of the transient extrudate swell and the comparison between jet buckling of UCM and Newtonian fluids.

MAGNETIC FIELD INDUCED NEAR-BAND-GAP OPTICAL PROPERTIES IN EuTe LAYERS

The magnetic response of the near-band-edge optical properties is studied in EuTe layers. In several magneto-optical experiments, the absorption and emission are described as well as the related Stokes shift. Specifically, we present the first experimental report of the photoluminescence excitation (PLE) spectrum in Faraday configuration. The PLE spectra shows to be related with the absorption spectra through the observation of resonance between the excitation light and the zero-field band-gap. A new emission line appears at 1.6 eV at a moderate magnetic field in the photoluminescence (PL) spectra. Furthermore, we examine the absorption and PL red-shift induced by the magnetic field in the light of the d-f exchange interaction energy involved in these processes. Whereas the absorption red-shift shows a quadratic dependence on the field, the PL red-shift shows a linear dependence which is explained by spin relaxation of the excited state.

Efficient solutions to robust, semi-implicit discretizations of the immersed boundary method

The immersed boundary method is a versatile tool for the investigation of flow-structure interaction. In a large number of applications, the immersed boundaries or structures are very stiff and strong tangential forces on these interfaces induce a well-known, severe time-step restriction for explicit discretizations. This excessive stability constraint can be removed with fully implicit or suitable semi-implicit schemes but at a seemingly prohibitive computational cost. While economical alternatives have been proposed recently for some special cases, there is a practical need for a computationally efficient approach that can be applied more broadly. In this context, we revisit a robust semi-implicit discretization introduced by Peskin in the late 1970s which has received renewed attention recently. This discretization, in which the spreading and interpolation operators are lagged. leads to a linear system of equations for the inter-face configuration at the future time, when the interfacial force is linear. However, this linear system is large and dense and thus it is challenging to streamline its solution. Moreover, while the same linear system or one of similar structure could potentially be used in Newton-type iterations, nonlinear and highly stiff immersed structures pose additional challenges to iterative methods. In this work, we address these problems and propose cost-effective computational strategies for solving Peskin`s lagged-operators type of discretization. We do this by first constructing a sufficiently accurate approximation to the system`s matrix and we obtain a rigorous estimate for this approximation. This matrix is expeditiously computed by using a combination of pre-calculated values and interpolation. The availability of a matrix allows for more efficient matrix-vector products and facilitates the design of effective iterative schemes. We propose efficient iterative approaches to deal with both linear and nonlinear interfacial forces and simple or complex immersed structures with tethered or untethered points. One of these iterative approaches employs a splitting in which we first solve a linear problem for the interfacial force and then we use a nonlinear iteration to find the interface configuration corresponding to this force. We demonstrate that the proposed approach is several orders of magnitude more efficient than the standard explicit method. In addition to considering the standard elliptical drop test case, we show both the robustness and efficacy of the proposed methodology with a 2D model of a heart valve. (C) 2009 Elsevier Inc. All rights reserved.

A Robust, Fully Adaptive Hybrid Level-Set/Front-Tracking Method for Two-Phase Flows with an Accurate Surface Tension Computation

We present a variable time step, fully adaptive in space, hybrid method for the accurate simulation of incompressible two-phase flows in the presence of surface tension in two dimensions. The method is based on the hybrid level set/front-tracking approach proposed in [H. D. Ceniceros and A. M. Roma, J. Comput. Phys., 205, 391400, 2005]. Geometric, interfacial quantities are computed from front-tracking via the immersed-boundary setting while the signed distance (level set) function, which is evaluated fast and to machine precision, is used as a fluid indicator. The surface tension force is obtained by employing the mixed Eulerian/Lagrangian representation introduced in [S. Shin, S. I. Abdel-Khalik, V. Daru and D. Juric, J. Comput. Phys., 203, 493-516, 2005] whose success for greatly reducing parasitic currents has been demonstrated. The use of our accurate fluid indicator together with effective Lagrangian marker control enhance this parasitic current reduction by several orders of magnitude. To resolve accurately and efficiently sharp gradients and salient flow features we employ dynamic, adaptive mesh refinements. This spatial adaption is used in concert with a dynamic control of the distribution of the Lagrangian nodes along the fluid interface and a variable time step, linearly implicit time integration scheme. We present numerical examples designed to test the capabilities and performance of the proposed approach as well as three applications: the long-time evolution of a fluid interface undergoing Rayleigh-Taylor instability, an example of bubble ascending dynamics, and a drop impacting on a free interface whose dynamics we compare with both existing numerical and experimental data.

Lie algebra methods for the applications to the statistical theory of turbulence

Approximate Lie symmetries of the Navier-Stokes equations are used for the applications to scaling phenomenon arising in turbulence. In particular, we show that the Lie symmetries of the Euler equations are inherited by the Navier-Stokes equations in the form of approximate symmetries that allows to involve the Reynolds number dependence into scaling laws. Moreover, the optimal systems of all finite-dimensional Lie subalgebras of the approximate symmetry transformations of the Navier-Stokes are constructed. We show how the scaling groups obtained can be used to introduce the Reynolds number dependence into scaling laws explicitly for stationary parallel turbulent shear flows. This is demonstrated in the framework of a new approach to derive scaling laws based on symmetry analysis [11]-[13].

Temperature Dynamics Investigation At Small And Shallow Lakes Using Hydrodynamic Model

A three-dimensional time-dependent hydrodynamic and heat transport model of Lake Binaba, a shallow and small dam reservoir in Ghana, emphasizing the simulation of dynamics and thermal structure has been developed. Most numerical studies of temperature dynamics in reservoirs are based on one- or two-dimensional models. These models are not applicable for reservoirs characterized with complex flow pattern and unsteady heat exchange between the atmosphere and water surface. Continuity, momentum and temperature transport equations have been solved. Proper assignment of boundary conditions, especially surface heat fluxes, has been found crucial in simulating the lake’s hydrothermal dynamics. This model is based on the Reynolds Average Navier-Stokes equations, using a Boussinesq approach, with a standard k − ε turbulence closure to solve the flow field. The thermal model includes a heat source term, which takes into account the short wave radiation and also heat convection at the free surface, which is function of air temperatures, wind velocity and stability conditions of atmospheric boundary layer over the water surface. The governing equations of the model have been solved by OpenFOAM; an open source, freely available CFD toolbox. As its core, OpenFOAM has a set of efficient C++ modules that are used to build solvers. It uses collocated, polyhedral numerics that can be applied on unstructured meshes and can be easily extended to run in parallel. A new solver has been developed to solve the hydrothermal model of lake. The simulated temperature was compared against a 15 days field data set. Simulated and measured temperature profiles in the probe locations show reasonable agreement. The model might be able to compute total heat storage of water bodies to estimate evaporation from water surface.

Simulação numérica de esteiras em transição utilizando o método dos contornos virtuais

Simulações Numéricas são executadas em um código numérico de alta precisão resolvendo as equações de Navier-Stokes e da continuidade para regimes de escoamento incompressíveis num contexto da turbulência bidimensional. Este código utiliza um esquema compacto de diferenças finitas de sexta ordem na aproximação das derivadas espaciais. As derivadas temporais são calculadas usando o esquema de Runge-Kuta de terceeira ordem com baixo armazenamento. Tal código numérico fornece uma representação melhorada para uma grande faixa de escalas de comprimento e de tempo. As técnicas dos contornos imersos acopladas ao método dos contornos virtuais permitem modelar escoamentos não-estacionários sobre geometrrias complexas, usando simplesmente uma malha Cartesiana uniforme. Por meio de procedimentos de aproximação/interpolação, as técnicas dos contornos imersos (aproximação Gaussiana, interpolação bilinear e redistribuição Gaussiana), permitem a representação do corpo sólido no interior do campo de escoamento, com a superfície não coincidindo com a malha computacional. O método dos contornos virtuais, proposto originalmente por Peskin, consiste, basicamente, na imposição na superfície e/ou no interior do corpo, de um termo de força temporal acrescentando às equações do momento. A aplicação deste campo de força local leva o fluido ao repouso na superfície do corpo, permitindo obter as condições de contorno de não-deslizamento e de não penetração de fluido na parede. A análise das oscilações induzidas no escoamento-contorno pelo processo de desprendimento de vórtices na esteira do cilindro circular e de geometria retangulares na incidência, para números de Reybolds variando de 40 a 400, confirma a eficiência computacional e a aplicabilidade das técncias implementadas.

Modelo matemático de um agitador eletromagnético

O objetivo deste trabalho é estudar os efeitos eletromagnéticos e fluido-dinâmicos induzidos no aço, decorrentes do uso de um agitador eletromagnético. Para tal, foi proposta a construção de um modelo numérico que resolva, de forma acoplada, os problemas de eletromagnetismo e fluido-dinâmica. O modelo numérico do problema eletromagnético, em elementos finitos, foi construído utilizando-se o software Opera-3d/Elektra da Vector Fields. O mesmo foi validado com medidas experimentais de densidade de fluxo magnético feitas na usina. O escoamento decorrente da agitação eletromagnética foi resolvido fazendo-se o acoplamento das forças de Lorentz com as equações de Navier-Stokes. Essas últimas foram resolvidas pelo método de volumes finitos, usando-se o software CFX-4 da AEA Technology. O modelo eletromagnético mostrou que existe um torque máximo dependente da freqüência do campo magnético. Também foi observado que a força magnética aumenta em quatro vezes seu valor, quando a corrente é duplicada. O perfil de escoamento produzido no molde, sob agitação eletromagnética, indica, que as situações de lingotamento testadas, não propiciam o arraste da escória. A velocidade crítica de arraste, determinada via modelo físico, não foi atingida para nenhum caso testado. O modelo fluido-dinâmico e térmico apresentou um aumento do fluxo de calor cedido pelo fluido para a casca solidificada com o uso do agitador eletromagnético. Como conseqüência, observou-se uma queda na temperatura do banho. Também foi observado, que o uso do agitador propicia a remoção de inclusões das camadas mais externas do tarugo. Ao mesmo tempo, notou-se que o uso do agitador aumenta o índice de remoção de inclusões para as duas seções de molde analisadas.

Síntese de novas bases de tröger, fluorescentes via transferência protônica intramolecular no estado excitado (ESIPT)

Neste trabalho, realizou-se a síntese e a caracterização de quatro novas bases de Tröger. Estes compostos pertencem à classe de heterociclos 2-hidroxifenibenzazóis, que caracterizam-se por apresentar uma forte emissão de fluorescência, devido à reação de transferência protônica intramolecular no estado excitado -ESIPT- por eles sofrrida quando excitados por luz ultravioleta. Os heterociclos sintetizadosapesentam ligações de hidrogênio intramolecular entrte o nitrogênio azólico e a hidroxila fenólica e um granded deslocamento de Stokes, características tíicas de compostos que sofrem a ESIPT. As bases de Tröger, que são quirais, são bem conhecidas como receptores moleculares devido a concavidade que estas moléculas apresentam, Os compostos obtidos são os primeiro exmeplos de bases de Tröger fluorescentes, via ESIP, na literatura, por isso, despertam grande interesse na síntese de sondas biológicas moleculares fluorescentes. A partir da resolução quiral das bases de Tröger, estas potencialmente podem vir a ser utilizadas como indutores quirais e/ou par ao reconhecimento enantiosseletivo do DNA. A resolução quiral foi feita para uma das bases de Tröger sintetizadas.

Síntese, caracterização e estudo fotofísico de heterociclos fluorescentes por ESIPT e suas aplicações na preparação de novos materiais

Neste trabalho é apresentada a síntese e a caracterização de compostos do tipo 2-(2'-hidroxifenil)benzazólicos, fluorescentes e com um grande deslocamento de Stokes, devido a um mecanismo de transferência protônica intramolecular no estado excitado (ESIPT). Estes derivados possuem a função amino, de grande versatilidade sintética. A possibilidade de aplicação dos compostos sintetizados foi testada em cinco diferentes sistemas. Os derivados foram utilizados como monômetros vinilênicos e acriloilamida para a polimerização com metacrilato de metila para a produção de novos materiais poliméricos orgânicos fluorescentes; como sondas fluorescentes para proteínas, marcando com sucesso albumina sérica bovina, apresentando conjugados com maior fotoestabilidade em relação a sondas comerciais; como uma molécula com propriedades altamente não-lineares, possuindo o maior valor para a primeira hiperpolarizabilidade conhecido até hoje; como ligante para a complexação com metais de transição. com potencial aplicação em dispositivos orgânicos emissores de luz, e como derivados silifuncionalizados para a obtenção de materiais híbridos através de reação sol-gel, e a partir destes, obter os primeiros aerogéis de sílica fluorescentes por ESIPT.