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General Information
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Head of Group: |
José Manuel Vega
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Research Area:
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Applied Mathematics
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Center involved:
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E.T.S.I. Aeronáuticos. UPM
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Plaza Cardenal Cisneros, 3
28040, Madrid, Spain
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Notice board
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Talk
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Spatially localized structures in one and
two dimensions
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Edgar Knobloch
Department of Physics,
University of California,
Berkeley, USA
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Abstract
Many continuum systems in physics exhibit a spatially localized
response to spatially homogeneous forcing. The resulting structures
are frequently called dissipative solitons. In this talk I will describe
the phenomenon of homoclinic snaking that is responsible for
the presence of these states, together with the associated snakesand-
ladders structure of the snaking region, i.e. the parameter region
containing such localized structures. I will describe different
types of snaking in both one and two spatial dimensions, focusing
on the manner in which localized structures grow as one follows the
solution branch from small to large amplitude. I will illustrate the
results using both model equations such as the Swift-Hohenberg
and forced Ginzburg-Landau equations, and "real" systems such
as binary fluid convection and magnetoconvection.
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[pdf]
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Date:
Thursday, January 12, 2012
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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Effects of Mistuning, Aerodynamics and
Cracks on the Dynamics of Multi-Stage
Bladed Disks
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Bodgan I. Epurenau
Department of Mechanical Engineering,
University of Michigan – Ann Arbor
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Abstract
Accurate modeling of realistic industrial turbomachinery requires
overcoming several challenges, including: (1) handling the complexity
of turbomachinery models, which often include multiple stages;
(2) modeling the aerodynamic loads; (3) modeling the nonlinear dynamics
caused by cracks in multi-stage systems. These challenges
are addressed in this talk. First, a methodology is presented to construct
reduced order models (ROMs) of multi-stage systems with
mistuning using single-sector calculations only. These ROMs are
then used to perform a statistical characterization of structural mistuning
in multi-stage systems, and to introduce a new classification
method for characterizing the properties of all modes. Next, the effects
of the aerodynamics on the multi-stage response are explored.
The methodology consists of first creating efficient structural ROMs,
and then iteratively calculating the aerodynamic stiffness matrices
for each stage. Finally, the effects of cracks are discussed. A novel
methodology for modeling the nonlinear vibration analysis of multistage
systems with mistuning and a cracked blade is proposed. The
nonlinear effects of a crack opening and closing are considered in
conjunction with the effects of mistuning. A variety of results are
provided for a two-stage industrial rotor, and the accuracy and efficiency
of the proposed methods are discussed.
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[pdf]
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Date:
Tuesday, September 20, 2011
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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On the numerical computation of complex resonances
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Thorsten Hohage
Institut für Numerische und Angewandte Mathematik,
Georg-August Universität Göttingen, Germany
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Abstract
Resonances can be defined as complex eigenvalues of a self-adjoint differential
operator on an unbounded domain, for which the corresponding eigenfunction
satisfies a radiation condition. Such eigenfunctions are typically highly improper
since they increase exponentially at infinity. Resonances appear in a variety of applications
including acoustics (e.g. musical instruments or slat noise in air-planes),
molecular dynamics, and optics (e.g. lasers or leaky modes in wave-guides). Excitation
of a resonant system by a resonant frequency (the square root of the real
part of a resonance) leads to a large system response, which can be approximately
computed with the help of the corresponding resonance and eigenfunction.
To compute such resonances numerically, we split the domain into a bounded
computational domain and an unbounded exterior domain. For the discretization
of the exterior domain we suggest so-called Hardy-space infinite elements, which
preserve the eigenvalue structure of the problem and exhibit super-algebraic convergence.
Their performance is illustrated by numerical simulations for acoustic
and electromagnetic resonance problems.
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[pdf]
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Date:
Friday, April 8, 2011
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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Control del calentamiento de piezas de
acero en hornos industriales: simulación
numérica y modelos reducidos
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Fernando Varas
Matemática Aplicada II, E.T.S.I. Telecomunicación,
Universidad de Vigo
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Abstract
La simulación numérica del calentamiento de piezas en hornos industriales presenta
grandes beneficios potenciales, tanto en el diseño de las condiciones de operación
como en el control de los hornos. Sin embargo, la complejidad del problema
hace inviable el uso de simulación numérica directa, salvo quizá en situaciones
muy concretas.
En esta charla se presenta la aplicación de modelos de orden reducido que
permiten trabajar ‘en tiempo real’ (entendiendo como tal un tiempo de cálculo compatible
con la implementación en un código de simulación de procesos o que se
encuentre por debajo de los tiempos característicos empleados en la estrategia de
control del horno).
Se considerarán dos casos concretos, relacionados con proyectos de carácter
industrial que se desarrollan actualmente en la Universidad de Vigo. El primero de
ellos se refiere a la predicción del calentamiento de ejes de automoción forjados
en un horno de tratamiento térmico (previo al baño de temple) en condiciones
estacionarias, con vistas al rediseño del horno y/o de su operación. El segundo
caso corresponde a la predicción del calentamiento de grandes piezas de acero
(para la alimentación de un tren de laminación en caliente) destinada a integrarse
en el esquema de regulación del horno.
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[pdf]
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Date:
Wednesday, February 2, 2011
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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A boundary integral biased introduction to
transparent boundary conditions for waves
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Francisco-Javier Sayas
Department of Mathematical Sciences,
University of Delaware
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Abstract
A relevant problem in the computational simulation of (time-harmonic and transient)
waves is the devising of the correct boundary conditions that allow us to
cut-off the computational domain and, therefore, to use any of the common PDE
solvers. The main issue arises from the fact that waves have to be allowed to scatter
away but the artificial boundary has to avoid them bouncing back.
This problem is nowadays very well understood in the time-harmonic case,
for the most relevant types of linear waves: acoustic, elastic, electromagnetic,...
Much recent progress is occurring in the field of transient problems. Most possible
approaches can be categorized in three classes (almost corresponding to
tribal groups): ABC, PML and BIE. I will try to explain the advantages and disadvantages
of some Absorbing Boundary Conditions and Perfectly Matched Layers
for transient acoustic waves. I will then move to the realm of Boundary Integral
Operators/Equations, explaining what they have to offer (exactness and arbitrary
closeness to where "stuff happens") and what is the price to pay, both at the computational
level and at the steep learning process they require.
The talk will be informative. There will be plenty of formulas and some pictures,
but no theorems or Sobolev spaces.
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[pdf]
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Date:
Tuesday, January 25, 2011
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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Computation of Invariant Tori and Periodic
Orbits by Multiple Shooting in Large-Scale
Dissipative Systems
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Juan Sánchez
Dept. Física Aplicada,
Universitat Politècnica de Catalunya
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Abstract
The invariant manifolds of a dynamical system are organizing centers, whose
computation and study help to understand its dynamics. The continuation of steady
solutions of parabolic systems of partial differential equations with respect to parameters
is now a common tool in Science and Engineering. The computation of
other invariant manifolds, such as periodic orbits and invariant tori is not so usual,
although all of them can be cast into a common framework, through the calculation
of fixed points of an appropriately defined map. Both the definition of the map and
the calculation of its fixed points through the Newton-Krylov method requires some
care, especially in the case of invariant tori.
The computation of periodic orbits by parallel multiple shooting will also be considered.
Codes using this method can achieve linear or close to linear speedups.
The MPI library has been used in our calculations but OMP could also be used on
architectures based on shared-memory multi-core processors.
As a test problem, the thermal convection of a binary fluid will be considered.
This is joint work with Marta Net and Carles Simò.
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[pdf]
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Date:
Friday, September 10, 2010
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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Lagrangiana de los flujos aperiódicos
Aplicaciones a flujos oceánicos
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Dra. Ana María Mancho
Dpto. de Matemáticas IMAFF,
Consejo Superior de Investigaciones Científicas
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Abstract
La teoría de los sistemas din´micos ha resultado exitosa para
describir el transporte por advección en fluidos. Sin embargo su
potencia se ve mermada por la falta de una teoría matemática
establecida para describir los sistemas dinámicos no autónomos.
En esta presentación introducir nuevos conceptos que generalizan
ideas bien asentadas de los sistemas dinámicos autónomos
y periódicos, al caso dependiente del tiempo de forma aperiódica.
Este es un problema de gran interés para la descripción del transporte
en flujos geofísicos. Se ilustrara la eficacia de estas herramientas
en el análisis de datos de altimetría, tomados sobre la
superficie oceánica en la región de la corriente de Kuroshio.
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[pdf]
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Date:
Lunes, 21 de junio de 2010
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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Aproximación numérica de problemas de
convección-difusión con convección
dominante
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Julia Novo
Departamento de Matemáticas,
Instituto de Ciencias Matemáticas CSIC-UAM-UC3M-UCM,
Universidad Autónoma de Madrid
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Abstract
Se consideran ecuaciones de evolución de tipo convección-difusión, en el caso
límite en que domina la convección. Es bien conocido que los métodos clásicos
de elementos finitos no son adecuados para aproximar problemas de convección
dominante.
En la primera parte de la charla se expone un procedimiento que permite eliminar
las oscilaciones espúreas de los métodos clásicos. Se propone también un
algoritmo adaptativo con el cual se obtiene una malla espacial automáticamente
adaptada sobre la cual la aproximación Galerkin no es oscilante.
En la segunda parte de la charla se estudia la aproximación numérica de las
mismas ecuaciones usando métodos de tipo ENO (essentially non oscillatory)
en espacio. Este tipo de métodos se usan con mucha frecuencia en el contexto
de la resolución de ecuaciones hiperbólicas. En este trabajo mostraremos que
estos métodos son también adecuados para resolver problemas de convecció-nreacción-
difusión en los que domina la convección. Nuevamente se propone un
procedimiento adaptativo en espacio para mejorar la eficiencia de los métodos
considerados.
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[pdf]
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Date:
Wednesday, September 22, 2010
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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Spatially localized patterns
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Edgar Knobloch
Department of Physics,
University of California,
Berkeley, USA
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Abstract
This talk will describe the origin and properties of spatially
localized structures in one and two dimensions using a model equation,
the Swift-Hohenberg equation, and will use this understanding to explain
the properties of similar structures recently identified in convection
and shear flows using both direct numerical simulations and numerical
branch-following.
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[pdf]
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Date:
Thursday January 14, 2010
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Torres Quevedo.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Research group presentation
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Summary of recent research activity
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Date:
Wednesday May 27, 2009
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Seminar
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Installation and basic description of the use of the CFD code elsA
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Date:
Friday February 27, 2009
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Location:
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Dpto. Fundamentos Matemáticos
E.T.S. Ingenieros Aeronáuticos. U.P.M.
Plaza Cardenal Cisneros, 3. 28040, Madrid
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Talk
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Nonlinear parabolized stability computations of the interaction between streamwise streaks and Tollmien-Schlichting waves
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Dr. Shervin Bagheri
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Abstract
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[pdf]
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Date:
Tuesday February 3, 2009
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Time:
12h 30'
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Location:
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E.T.S. Ingenieros Aeronáuticos. U.P.M.
Aula Magna (edificio 2).
Plaza Cardenal Cisneros, 3. 28040, Madrid
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[
Fundamentos Matemáticos
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E.T.S.I.A.
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U.P.M.
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