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Extended analysis of a pseudo-spectral approach to the vortex patch problemBertolino, Mattias January 2018 (has links)
A prestudy indicated superior accuracy and convergence properties of apseudo-spectral method compared to a spline-based method implemented byCòrdoba et al. in 2005 when solving the α-patches problem. In this thesis wefurther investigate the numerical properties of the pseudo-spectral method and makeit more robust by implementing the Nonequispaced Fast Fourier Transform. Wepresent a more detailed overview and analysis of the pseudo-spectral method and theα-patches problem in general and conclude that the pseudo-spectral method issuperior in regards to accuracy in periodic settings.
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Estudo da aplicabilidade do método de fronteira imersa no cálculo de derivadas de Flutter com as equações de Euler para fluxo compressível / Study of the applicability of the immersed boundary method in the calculation of the nonstationary aerodynamics derivatives for flutter analysis using the Euler equations for compressible flowJosé Laércio Doricio 08 June 2009 (has links)
Neste trabalho, desenvolve-se um método de fronteira imersa para o estudo de escoamento compressível modelado pelas equações de Euler bidimensionais. O método de discretização de diferenças finitas é empregado, usando o método de Steger-Warming de ordem dois para discretizar as variáveis espaciais e o esquema de Runge-Kutta de ordem quatro para discretizar as variáveis temporais. O método da fronteira imersa foi empregado para o estudo de aeroelasticidade computacional em uma seção típica de aerofólio bidimensional com dois movimentos prescritos: torsional e vertical, com o objetivo de se verifcar a eficiência do método e sua aplicabilidade para problemas em aeroelasticidade computacional. Neste estudo desenvolveu-se também um programa de computador para simular escoamentos compressíveis de fluido invíscido utilizando a metodologia proposta. A verificação do código gerado foi feita utilizando o método das soluções manufaturadas e o problema de reflexão de choque oblíquo. A validação foi realizada comparando-se os resultados obtidos para o escoamento ao redor de uma seção circular e de uma seção de aerofólio NACA 0012 com os resultados experimentais, para cada caso. / In this work, an immersed boundary method is developed to study compressible flow modeled by the two-dimensional Euler equations. The finite difference method is employed, using the second order Steger-Warming method to discretizate the space variables and the fourth order Runge-Kutta method to discretizate the time variables. The immersed boundary method was employed to study computational aeroelasticity on a typical two-dimensional airfoil section with two prescribed motion: pitching and plunging, in order to verify the efficiency of the numerical method and its applicability in computational aeroelasticity problems. In this work, a computer program was developed to simulate compressible flows for inviscid fluids using the methodology proposed. The verification of the computational code was performed using the method of manufactured solutions and the oblique shock wave reflection problem. The validation was performed comparing the obtained results for flows around a circular section and a NACA 0012 airfoil section with the experimental results, for each case.
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Schémas numériques pour la simulation de l'explosion / numerical schemes for explosion hazardsTherme, Nicolas 10 December 2015 (has links)
Dans les installations nucléaires, les explosions, qu’elles soient d’origine interne ou externe, peuvent entrainer la rupture du confinement et le rejet de matières radioactives dans l’environnement. Il est donc fondamental, dans un cadre de sûreté de modéliser ce phénomène. L’objectif de cette thèse est de contribuer à l’élaboration de schémas numériques performants pour résoudre ces modèles complexes. Les travaux présentés s’articule autour de deux axes majeurs : le développement de schémas volumes finis consistants pour les équations d’Euler compressible qui modélise les ondes de choc et celui de schémas performants pour la propagation d’interfaces comme le front de flamme lors d'une déflagration. La discrétisation spatiale est de type mailles décalées pour tous les schémas développés. Les schémas pour les équations d'Euler se basent sur une formulation en énergie interne qui permet de préserver sa positivité ainsi que celle de la masse volumique. Un bilan d'énergie cinétique discret peut être obtenu et permet de retrouver un bilan d'énergie totale par l'ajout d'un terme de correction dans le bilan d'énergie interne. Le schéma ainsi construit est consistant au sens de Lax avec les solutions faibles entropiques des équations continues. On utilise les propriétés des équations de type Hamilton-Jacobi pour construire une classe de schémas volumes finis performants sur une large variété de maillages modélisant la propagation du front de flamme. Ces schémas garantissent un principe du maximum et possèdent des propriétés importantes de monotonie et consistance qui permettent d'obtenir un résultat de convergence. / In nuclear facilities, internal or external explosions can cause confinement breaches and radioactive materials release in the environment. Hence, modeling such phenomena is crucial for safety matters. The purpose of this thesis is to contribute to the creation of efficient numerical schemes to solve these complex models. The work presented here focuses on two major aspects: first, the development of consistent schemes for the Euler equations which model the blast waves, then the buildup of reliable schemes for the front propagation, like the flame front during the deflagration phenomenon. Staggered discretization is used in space for all the schemes. It is based on the internal energy formulation of the Euler system, which insures its positivity and the positivity of the density. A discrete kinetic energy balance is derived from the scheme and a source term is added in the discrete internal energy balance equation to preserve the exact total energy balance. High order, MUSCL-like interpolators are used in the discrete momentum operators. The resulting scheme is consistent (in the sense of Lax) with the weak entropic solutions of the continuous problem. We use the properties of Hamilton-Jacobi equations to build a class of finite volume schemes compatible with a large number of meshes to model the flame front propagation. These schemes satisfy a maximum principle and have important consistency and monotonicity properties. These latters allows to derive a convergence result for the schemes based on Cartesian grids.
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Direct Numerical Simulations of Fluid Turbulence : (A) Statistical Properties of Tracer And Inertial Particles (B) Cauchy-Lagrange Studies of The Three Dimensional Euler EquationBhatnagar, Akshay January 2016 (has links) (PDF)
The studies of particles advected by tubulent flows is an active area of research
across many streams of sciences and engineering, which include astrophysics,
fluid mechanics, statistical physics, nonlinear dynamics, and also chemistry and biology. Advances in experimental techniques and high performance computing have made it possible to investigate the properties these
particles advected by fluid flows at very high Reynolds numbers. The main focus of this thesis is to study the statistics of Lagrangian tracers and heavy inertial particles in hydrodynamic and magnetohydrodynamic (MHD) turbulent
flows by using direct numerical simulations (DNSs). We also study the statistics of particles in model stochastic flows; and we compare our results for such models with those that we obtain from DNSs of hydrodynamic equations. We uncover some of aspects of the statistical properties of particle trajectories that have not been looked at so far. In the last part of the thesis we present some results that we have obtained by solving the three-dimensional
Euler equation by using a new method based on the Cauchy-Lagrange formulation. This thesis is divided into 6 chapters. Chapter 1 contains an introduction
to the background material that is required for this thesis; it also contains an
outline of the problems we study in subsequent Chapters. Chapter 2 contains
our study of “Persistence and first-passage time problems with particles in
three-dimensional, homogeneous, and isotropic turbulence”. Chapter 3 is devoted
to our study of “Universal Statistical Properties of Inertial-particle Trajectories
in Three-dimensional, Homogeneous, Isotropic, Fluid Turbulence”.
Chapter 4 deals with “Time irreversibility of Inertial-particle trajectories in
Homogeneous, Isotropic, Fluid Turbulence”. Chapter 5 contains our study
of the “Statistics of charged inertial particles in three-dimensional magnetohydrodynamic (MHD) turbulence”. Chapter 6 is devoted to our study of
“The Cauchy-Lagrange method for the numerical integration of the threedimensional
Euler equation”.
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Modélisation MHD et simulation numérique par des méthodes volumes finis. Application aux plasmas de fusion / MHD modeling and numerical simulation with finite volume-type methods. Application to fusion plasmaEstibals, Élise 02 May 2017 (has links)
Ce travail traite de la modélisation des plasmas de fusion qui est ici abordée à l'aide d'un modèle Euler bi-températures et du modèle de la magnétohydrodynamique (MHD) idéale et résistive. Ces modèles sont tout d'abord établis à partir des équations de la MHD bi-fluide et nous montrons qu'ils correspondent à des régimes asymptotiques différents pour des plasmas faiblement ou fortement magnétisés. Nous décrivons ensuite les méthodes de volumes finis pour des maillages structurés et non-structurés qui ont été utilisées pour approcher les solutions de ces modèles. Pour les trois modèles mathématiques étudiés dans cette thèse, les méthodes numériques reposent sur des schémas de relaxation. Afin d'appliquer ces méthodes aux problèmes de fusion par confinement magnétique, nous décrivons comment modifier les méthodes de volumes finis pour les appliquer à des problèmes formulés en coordonnées cylindriques tout en gardant une formulation conservative forte des équations. Enfin nous étudions une stratégie pour maintenir la contrainte de divergence nulle du champ magnétique qui apparait dans les modèles MHD. Une série de cas tests numériques pour les trois modèles est présentée pour différentes géométries afin de valider les méthodes numériques proposées. / This work deals with the modeling of fusion plasma which is discussed by using a bi-temperature Euler model and the ideal and resistive magnetohydrodynamic (MHD) ones. First, these models are established from the bi-fluid MHD equations and we show that they correspond to different asymptotic regimes for lowly or highly magnetized plasma. Next, we describe the finite volume methods for structured and non-structured meshes which have been used to approximate the solution of these models. For the three mathematical models studied in this thesis, the numerical methods are based on relaxation schemes. In order to apply those methods to magnetic confinement fusion problems, we explain how to modify the finite volume methods to apply it to problem given in cylindrical coordinates while keeping a strong conservative formulation. Finally, a strategy dealing with the divergence-free constraint of the magnetic field is studied. A set of numerical tests for the three models is presented for different geometries to validate the proposed numerical methods.
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Modélisation d'écoulements fluides en milieu encombré d'obstacles / Modeling fluid flows in obstructed mediaMartin, Xavier 24 November 2015 (has links)
On s'intéresse dans ce document à la modélisation d'écoulements compressibles en conduite unidimensionnelle (1D) à section variable et dans des domaines bi ou tridimensionnelles encombrés d'obstacles. Le travail est motivé par la modélisation d'écoulements dans les circuits de refroidissement de réacteurs à eau pressurisée (REP). Ainsi ce travail a pour objectif de proposer une nouvelle formulation pour de tels écoulements. L'idée de base consiste a utiliser une formulation intégrale sur la base des équations aux dérivées partielles. Le système de lois de conservation associé aux équations d'Euler (masse, dynamique et énergie) est examiné.Le premier chapitre examine le cas de conduite 1D à section continue ou discontinue. La formulation intégrale est présentée et les résultats numériques sont comparés avec (i) l'approche Well-Balanced et (ii) la solution de référence obtenue sur maillage très fin.Les second et troisième chapitres examinent la modélisation d'écoulements compressibles dans des domaines contenant de nombreux tubes. La formulation intégrale est donnée, et les schémas numériques présentés, afin de gérer les interfaces fluide/fluide et les parois. Les schémas peuvent être explicites (chapitre 2), ou implicites (chapitre 3). Quelques cas tests analytiques sont présentés. On se concentre sur l'écoulement d'un fluide abordant une zone de tubes alignés de petite taille. Ici encore, la comparaison est faite avec la référence fluide; les résultats sont également comparés avec ceux issus de l'approche équilibre classique, et ceux associés à la formulation intégrale unidimensionnelle présentée dans le premier chapitre. / This document focuses on the modeling of compressible flows in one-dimensional (1D) pipes with variable cross-section, and in two or three-dimensional domains containing many small obstacles. The basic motivation is urged by the modeling of flows in the coolant circuit of pressurised water reactors (PWR). Thus this work aims at providing a new formulation for such a variety of flows. The basic idea consists in using an integral approach that is applied to the governing set of partial differential equations. Here the keystone is the conservative Euler set of equations, including mass, momentum and energy balance for any equation of state.Hence, the first chapter investigates the case of one-dimensional pipes with continuous or discontinuous cross-section. Once the 1D+ integral formulation has been presented, numerical results are compared with : (i) the classical Well-Balanced (WB) approach, and (ii) the reference solution obtained with a multi-dimensional code with huge mesh refinement.The second and third chapters provide some new insight on the numerical modeling of compressible flows in domains obstructed with many tubes. The integral formulation is derived, and numerical schemes are detailed, in order to handle fluid/fluid interfaces and wall boundaries. Schemes may be explicit (chapter 2), or implicit (chapter 3). A few analytic test cases are investigated. Focus is made on the flow incoming a region containing many tiny and aligned tubes. Here again, a comparison with the reference "fluid" solution is achieved; results are also compared with those arising from the WB approach, and with those coming from the 1D+ integral approach proposed in the first chapter.
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Řešení problémů aeroakustiky pomocí bezsíťových metod / Meshfree methods for computational aeroacousticsBajko, Jaroslav January 2013 (has links)
Bezsíťové metody reprezentují alternativu ke standardním diskretizačním technikám, které pro svůj chod vyžadují síť. V posledních desetiletích bylo vynaloženo mnoho úsilí k ověření konkurenceschopnosti bezsíťových metod v různých inženýrských odvětvích. Diplomová práce je zaměřena na aplikaci vhodné bezsíťové metody ve výpočetní aeroakustice. Stěžejní část této práce se zabývá úlohami šíření zvuku, které lze modelovat pomocí linearizovaných Eulerových rovnic. Obecně lze tyto rovnice zařadit mezi lineární hyperbolické systémy. Pro úlohy aeroakustiky se jako vhodná bezsíťová metoda jeví Finite point method (FPM), která byla úspěšně použita pro řešení úloh dynamiky tekutin. Odvozením této metody a návrhy k dosažení vysoké přesnosti se věnuje další část práce. Úlohy šíření zvuku se známým řešením jsou testovány vlastním softwarem vyvinutým speciálně pro tyto účely.
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Schémas volumes finis à mailles décalées pour la dynamique des gaz / Finite volume schemes on staggered grids for gas dynamicsLlobell, Julie 24 October 2018 (has links)
L'objectif de cette thèse est de développer un nouveau schéma numérique du type volumes finis pour la dynamique des gaz. Dans deux articles, F.Berthelin, T.Goudon et S.Minjeaud proposent de résoudre le système des équations d'Euler barotrope en dimension 1 d'espace, avec un schéma d'ordre 1 fonctionnant sur grilles décalées et dont la conception des flux est inspirée des schémas cinétiques. Nous proposons d'enrichir ce schéma afin qu'il puisse résoudre le système des équations d'Euler barotrope ou complet, en dimension 2 d'espace sur maillage cartésien ou non structuré, possiblement à l'ordre 2 et le cas échéant à bas nombres de Mach. Nous commencerons par développer une version 2D du schéma sur grilles cartésiennes (ou MAC) à l’ordre 2 via une méthode de type MUSCL, d'abord pour les équations barotropes puis pour les équations complètes. Ces dernières demandent de traiter une équation d’énergie supplémentaire et l’un des problèmes -résolu- est de trouver une définition discrète convenable de l’énergie totale telle qu'elle satisfasse une équation conservative locale. Dans un troisième chapitre nous étudierons le passage à la limite du compressible vers l'incompressible et nous verrons comment utiliser les atouts de notre schéma afin de le modifier et d'en faire un schéma Asymptotic Preserving pour des écoulements à bas nombres de Mach. Dans un quatrième temps nous proposerons une adaptation du schéma sur des maillages non structurés. Notre approche sera fortement inspirée des méthodes DDFV et pourra présenter des avantages dans les régimes à faibles nombres de Mach. Cette thèse se termine par un cinquième chapitre issu d’une collaboration lors du CEMRACS 2017, où le point de vue considéré n’est plus macroscopique mais microscopique. Nous commencerons par étudier un modèle micro/macro idéalisé auquel un processus stochastique a été ajouté puis nous tenterons d'en déduire un modèle à grande échelle pour un système fortement couplé, qui soit consistant avec la description micro/macro sous-jacente du problème physique. / The objective of this thesis is to develop a new numerical scheme of finite volume type for gas dynamics. In two articles, F.Berthelin, T.Goudon and S.Minjeaud propose to solve the barotropic Euler system in dimension 1 of space, with a first order scheme that works on staggered grids and of which fluxes are inspired by kinetic schemes. We propose to enhance this scheme so that it can solve the barotropic or complete Euler systems, in dimension 2 of space on Cartesian or unstructured grids, possibly at order 2 and at Low Mach numbers where appropriate. We begin with the development of a 2D version of the scheme on Cartesian (or MAC) grids, at order 2 via a MUSCL type method, for the barotropic equations at first and then for the complete equations. The latter require to handle with an additional energy equation and one of the -solved- problems is to find a suitable discrete definition of the total energy such that it satisfies a local conservative equation. In a third chapter we study the transition from the compressible case to the incompressible limit and we shall see how to use the advantages of our initial scheme in order to make it an Asymptotic Preserving scheme at low Mach numbers. In a fourth chapter we propose an adaptation of the scheme on unstructured meshes. Our approach is strongly inspired by the DDFV methods and may have advantages in low-Mach regimes.This thesis ends with a fifth chapter issued from a collaboration during CEMRACS 2017, where the considered point of view is no longer macroscopic but microscopic. We begin by studying a simplified micro/macro model with an added stochastic process and then we attempt to deduce a large-scale model for a strongly coupled system which has to be consistent with the underlying micro / macro description of the physical problem.
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Onsager's ConjectureBuckmaster, Tristan 22 August 2014 (has links)
In 1949, Lars Onsager in his famous note on statistical hydrodynamics conjectured that weak solutions to the 3-D incompressible Euler equations belonging to Hölder spaces with Hölder exponent greater than 1/3 conserve kinetic energy; conversely, he conjectured the existence of solutions belonging to any Hölder space with exponent less
than 1/3 which do not conserve kinetic energy. The first part, relating to conservation of kinetic energy, has since been confirmed (cf. Eyink 1994, Constantin-E-Titi 1994). The second part, relating to the existence of non-conservative solutions, remains an open conjecture and
is the subject of this dissertation.
In groundbreaking work of De Lellis and Székelyhidi Jr. (2012), the
authors constructed the first examples of non-conservative Hölder continuous weak solutions to the Euler equations. The construction was subsequently improved by Isett (2012/2013), introducing many novel ideas in order to construct 1/5− Hölder continuous weak solutions with compact support in time.
Adhering more closely to the original scheme of De Lellis and Székelyhidi Jr., we present a comparatively simpler construction of 1/5− Hölder continuous non-conservative weak solutions which may in addition be made to obey a prescribed kinetic energy profile. Furthermore, we extend this scheme in order to construct weak non-conservative solutions to the Euler equations whose Hölder 1/3− norm is Lebesgue integrable in time.
The dissertation will be primarily based on three papers, two of which being in collaboration with De Lellis and Székelyhidi Jr.
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Adaptivní hp nespojitá Galerkinova metoda pro nestacionární stlačitelné Eulerovy rovnice / Adaptivní hp nespojitá Galerkinova metoda pro nestacionární stlačitelné Eulerovy rovniceKorous, Lukáš January 2012 (has links)
The compressible Euler equations describe the motion of compressible inviscid fluids. They are used in many areas ranging from aerospace, automotive, and nuclear engineering to chemistry, ecology, climatology, and others. Mathematically, the compressible Euler equations represent a hyperbolic system consisting of several nonlinear partial differential equations (conservation laws). These equations are solved most frequently by means of Finite Volume Methods (FVM) and low-order Finite Element Methods (FEM). However, both these approaches are lacking higher order accuracy and moreover, it is well known that conforming FEM is not the optimal tool for the discretization of first-order equations. The most promissing approach to the approximate solution of the compressible Euler equations is the discontinuous Galerkin method that combines the stability of FVM, with excellent approximation properties of higher-order FEM. The objective of this Master Thesis was to develop, implement and test new adaptive algorithms for the nonstationary compressible Euler equations based on higher-order discontinuous Galerkin (hp-DG) methods. The basis for the new methods were the discontinuous Galerkin methods and space-time adaptive hp-FEM algorithms on dynamical meshes for nonstationary second-order problems. The new algorithms...
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