<?xml version="1.0" encoding="UTF-8"?>
<rss xmlns:itunes="http://www.itunes.com/dtds/podcast-1.0.dtd" xmlns:dc="http://purl.org/dc/elements/1.1/" version="2.0">
  <channel>
    <title>DSpace Collection:</title>
    <link>http://hdl.handle.net/2117/3193</link>
    <description />
    <pubDate>Sun, 19 May 2013 18:20:00 GMT</pubDate>
    <dc:date>2013-05-19T18:20:00Z</dc:date>
    <itunes:owner>
      <itunes:email>webmaster.bupc@upc.edu</itunes:email>
      <itunes:name>Universitat Politècnica de Catalunya. Servei de Biblioteques i Documentació</itunes:name>
    </itunes:owner>
    <itunes:explicit>no</itunes:explicit>
    <itunes:keywords />
    <item>
      <title>Numerical simulation of wrap scroll temperature for refrigeration and air conditioning compressors</title>
      <link>http://hdl.handle.net/2117/18870</link>
      <description>Title: Numerical simulation of wrap scroll temperature for refrigeration and air conditioning compressors
Authors: Rovira Casals, Jordi; Rigola Serrano, Joaquim; Pérez Segarra, Carlos David; Oliva Llena, Asensio
Abstract: Being part of a model which simulates the whole consecutive overall compression process in a scroll compressor by solving equations of mass, momentum and energy balance for fluid refrigerant (Rovira et al. ,2006), an updated version is presented. In this new model, an energy balance over the scroll wraps is implemented; where temperatures and heat fluxes are obtain&#xD;
ed dividing the wall into 36 parts (slices) each turn.&#xD;
The scroll wrap is divided into different solid slices; energy balance is carried out, taking into account: i) conduction along the scroll wrap; ii) convection heat transfer between each slice and each fluid chamber, with special attention&#xD;
on solid slice - fluid chamber contact at each time step. The numerical model shows the one dimensional and transient temperature, pressure and mass flow rate, at each fluid chamber along the scroll compressor, among detailed solid wrap temperature distribution.&#xD;
The whole numerical model has been experimentally validated against experimental data from technical literature (Halm,1997)(Chen et al.,2004a)(Chen et al.,2004b), comparing mass flow rate, discharge temperature, compression work and power consumption.&#xD;
Finally, the influence of wall temperatures and wall heat fluxes on the compressor performance and other output variables is analyzed.</description>
      <pubDate>Thu, 18 Apr 2013 13:51:51 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/18870</guid>
      <dc:date>2013-04-18T13:51:51Z</dc:date>
      <itunes:author>Rovira Casals, Jordi; Rigola Serrano, Joaquim; Pérez Segarra, Carlos David; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>Being part of a model which simulates the whole consecutive overall compression process in a scroll compressor by solving equations of mass, momentum and energy balance for fluid refrigerant (Rovira et al. ,2006), an updated version is presented. In this new model, an energy balance over the scroll wraps is implemented; where temperatures and heat fluxes are obtain&#xD;
ed dividing the wall into 36 parts (slices) each turn.&#xD;
The scroll wrap is divided into different solid slices; energy balance is carried out, taking into account: i) conduction along the scroll wrap; ii) convection heat transfer between each slice and each fluid chamber, with special attention&#xD;
on solid slice - fluid chamber contact at each time step. The numerical model shows the one dimensional and transient temperature, pressure and mass flow rate, at each fluid chamber along the scroll compressor, among detailed solid wrap temperature distribution.&#xD;
The whole numerical model has been experimentally validated against experimental data from technical literature (Halm,1997)(Chen et al.,2004a)(Chen et al.,2004b), comparing mass flow rate, discharge temperature, compression work and power consumption.&#xD;
Finally, the influence of wall temperatures and wall heat fluxes on the compressor performance and other output variables is analyzed.</itunes:summary>
    </item>
    <item>
      <title>Numerical simulation of the turbulent fluid flow through valves based on low mach models</title>
      <link>http://hdl.handle.net/2117/18868</link>
      <description>Title: Numerical simulation of the turbulent fluid flow through valves based on low mach models
Authors: Rigola Serrano, Joaquim; Lehmkuhl Barba, Oriol; Ventosa, Jordi; Pérez Segarra, Carlos David; Oliva Llena, Asensio
Abstract: The aim of the present paper is to carry out a group of numerical experiments over the fluid flow through the valve reed, using the CFD&amp;HT code TermoFluids, an unstructure d and parallel object-oriented CFD code for accurate and reliable solving of industrial flows (Lehmkuhl, O. et al. 2007&#xD;
) with special attention on incompressible hypothesis against low Mach compressible flow modeling, as a critic al numerical aspect depending on Reynolds number and gap thickness conditions.&#xD;
In all studied cases a multi-dimensional explicit finite volume fractional-step based algorithm extended to simulate low Mach fluxes using a Runge-Kutta/Crank-Nicholson time integration scheme, with a symmetry preserving&#xD;
discretization has been used. When turbulence modeling is needed, an extension of the WALE (Wall Adapting Local Eddy-viscosity) (Nicoud, F. and Ducros, F., 1999) model to non-structured meshes is applied. The pressure&#xD;
equation is solved by means of parallel Fourier Schur decomposition solver which is an efficient direct solver for loosely coupled PC clusters (Borrell, R. et al. 2011). In a two dimensional periodic way the fluid flow is approach&#xD;
ed by two parallel phenomena (an entrance flow through a channel and a free jet through a surface). In that sense, the present paper is focused on the numeri&#xD;
cal simulation model of the fluid flow through the valve reeds, considering a simplified geometry of an axial hole plus a radial diffuser.&#xD;
The numerical results presented are based on a specific geome try – valve diameter D is 3 times orifice diameter d, while s/d ratio is 0.6 – considering high Reynolds number at the entrance as boundary condition. The studied cases show the influence from laminar to turbulent flow from incompressible assumption to lower subsonic conditions and/or chocked flow.</description>
      <pubDate>Thu, 18 Apr 2013 13:32:40 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/18868</guid>
      <dc:date>2013-04-18T13:32:40Z</dc:date>
      <itunes:author>Rigola Serrano, Joaquim; Lehmkuhl Barba, Oriol; Ventosa, Jordi; Pérez Segarra, Carlos David; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The aim of the present paper is to carry out a group of numerical experiments over the fluid flow through the valve reed, using the CFD&amp;HT code TermoFluids, an unstructure d and parallel object-oriented CFD code for accurate and reliable solving of industrial flows (Lehmkuhl, O. et al. 2007&#xD;
) with special attention on incompressible hypothesis against low Mach compressible flow modeling, as a critic al numerical aspect depending on Reynolds number and gap thickness conditions.&#xD;
In all studied cases a multi-dimensional explicit finite volume fractional-step based algorithm extended to simulate low Mach fluxes using a Runge-Kutta/Crank-Nicholson time integration scheme, with a symmetry preserving&#xD;
discretization has been used. When turbulence modeling is needed, an extension of the WALE (Wall Adapting Local Eddy-viscosity) (Nicoud, F. and Ducros, F., 1999) model to non-structured meshes is applied. The pressure&#xD;
equation is solved by means of parallel Fourier Schur decomposition solver which is an efficient direct solver for loosely coupled PC clusters (Borrell, R. et al. 2011). In a two dimensional periodic way the fluid flow is approach&#xD;
ed by two parallel phenomena (an entrance flow through a channel and a free jet through a surface). In that sense, the present paper is focused on the numeri&#xD;
cal simulation model of the fluid flow through the valve reeds, considering a simplified geometry of an axial hole plus a radial diffuser.&#xD;
The numerical results presented are based on a specific geome try – valve diameter D is 3 times orifice diameter d, while s/d ratio is 0.6 – considering high Reynolds number at the entrance as boundary condition. The studied cases show the influence from laminar to turbulent flow from incompressible assumption to lower subsonic conditions and/or chocked flow.</itunes:summary>
    </item>
    <item>
      <title>Modular simulation of vapour compression systems with an object oriented tool</title>
      <link>http://hdl.handle.net/2117/18866</link>
      <description>Title: Modular simulation of vapour compression systems with an object oriented tool
Authors: Ablanque Mejía, Nicolás; Oliet Casasayas, Carles; Rigola Serrano, Joaquim; Lehmkuhl Barba, Oriol; Pérez Segarra, Carlos David
Abstract: The objective of this work is to simulate vapour compression refrigeration systems through a modular approach by means of an object - oriented numerical tool called NEST. For this purpose, the global system is modeled&#xD;
as a collection of different elements which are linked between them.&#xD;
Each element represents a specific part of the system (e.g. heat exchanger,&#xD;
compressor, expansion device, tube, cavity, wall, etc.) and can be independently solved for given boundary conditions. The global resolution procedure is carried out by solving all the elements iteratively, transferring information between them, until a converged solution is reached.&#xD;
The system is easily modified by adding, subtracting or substituting any of&#xD;
its elements. This feature gives great flexibility to the model, not only&#xD;
because the configuration of the system can be clearly altered, but also because the numerical model of any element can be easily replaced allowing different levels of simulation. In this work the object - oriented methodology together with the elements description and their resolution procedures are presented. The model is validated against experimental data obtained from a refrigeration cycle working with isobutane. In addition to this, an illustrative case is presented in order to show the system capabilities.</description>
      <pubDate>Thu, 18 Apr 2013 13:12:59 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/18866</guid>
      <dc:date>2013-04-18T13:12:59Z</dc:date>
      <itunes:author>Ablanque Mejía, Nicolás; Oliet Casasayas, Carles; Rigola Serrano, Joaquim; Lehmkuhl Barba, Oriol; Pérez Segarra, Carlos David</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The objective of this work is to simulate vapour compression refrigeration systems through a modular approach by means of an object - oriented numerical tool called NEST. For this purpose, the global system is modeled&#xD;
as a collection of different elements which are linked between them.&#xD;
Each element represents a specific part of the system (e.g. heat exchanger,&#xD;
compressor, expansion device, tube, cavity, wall, etc.) and can be independently solved for given boundary conditions. The global resolution procedure is carried out by solving all the elements iteratively, transferring information between them, until a converged solution is reached.&#xD;
The system is easily modified by adding, subtracting or substituting any of&#xD;
its elements. This feature gives great flexibility to the model, not only&#xD;
because the configuration of the system can be clearly altered, but also because the numerical model of any element can be easily replaced allowing different levels of simulation. In this work the object - oriented methodology together with the elements description and their resolution procedures are presented. The model is validated against experimental data obtained from a refrigeration cycle working with isobutane. In addition to this, an illustrative case is presented in order to show the system capabilities.</itunes:summary>
    </item>
    <item>
      <title>Parallelization of the coupling between CFD models for airflow and building energy simulation with an object-oriented infrastructure</title>
      <link>http://hdl.handle.net/2117/18233</link>
      <description>Title: Parallelization of the coupling between CFD models for airflow and building energy simulation with an object-oriented infrastructure
Authors: Damle, Rashmin; Lehmkuhl Barba, Oriol; López Mas, Joan; Rigola Serrano, Joaquim; Oliva Llena, Asensio
Abstract: Integrating CFD &amp; HT models with the general building program raises the computational time of building simulations as these simulations are usually performed over a period of one year. Within this context, our aim is to&#xD;
couple a object-oriented modular building program with CFD &amp; HT for airflow and parallelize the simulation with numerous processors for reducing computational time. Also the modular nature of the code will allow to resolve&#xD;
selective critical zones with CFD &amp; HT models while employing simple models for airflow in less critical zones. Thus, there are different levels of modelling different rooms/elements of the building system depending on the requirements of a specific case.</description>
      <pubDate>Tue, 12 Mar 2013 16:34:32 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/18233</guid>
      <dc:date>2013-03-12T16:34:32Z</dc:date>
      <itunes:author>Damle, Rashmin; Lehmkuhl Barba, Oriol; López Mas, Joan; Rigola Serrano, Joaquim; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>Integrating CFD &amp; HT models with the general building program raises the computational time of building simulations as these simulations are usually performed over a period of one year. Within this context, our aim is to&#xD;
couple a object-oriented modular building program with CFD &amp; HT for airflow and parallelize the simulation with numerous processors for reducing computational time. Also the modular nature of the code will allow to resolve&#xD;
selective critical zones with CFD &amp; HT models while employing simple models for airflow in less critical zones. Thus, there are different levels of modelling different rooms/elements of the building system depending on the requirements of a specific case.</itunes:summary>
    </item>
    <item>
      <title>Combined heat and moisture transfer in buildings systems</title>
      <link>http://hdl.handle.net/2117/18220</link>
      <description>Title: Combined heat and moisture transfer in buildings systems
Authors: Damle, Rashmin; Lehmkuhl Barba, Oriol; Rigola Serrano, Joaquim; Oliva Llena, Asensio
Abstract: Temperature and humidity are the two main parameters indicating the comfort level of the building occupants. Although the effect of temperature is taken into account in thermal simulation of buildings, the moisture transfer through the rooms and porous building walls is sometimes neglected. The level of humidity can give different sensations of thermal comfort. It is necessary to take into account both heat and moisture transport in and around buildings to predict the hygrothermal behavior of rooms and building walls so as to calculate the energy demands correctly. In this work some benchmark exercises are worked out to see the performance of the heat and moisture transfer model implemented for rooms and porous walls. Finally, numerical results are compared with the measured data for a room exposed to varying outdoor conditions.</description>
      <pubDate>Tue, 12 Mar 2013 15:10:08 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/18220</guid>
      <dc:date>2013-03-12T15:10:08Z</dc:date>
      <itunes:author>Damle, Rashmin; Lehmkuhl Barba, Oriol; Rigola Serrano, Joaquim; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>Temperature and humidity are the two main parameters indicating the comfort level of the building occupants. Although the effect of temperature is taken into account in thermal simulation of buildings, the moisture transfer through the rooms and porous building walls is sometimes neglected. The level of humidity can give different sensations of thermal comfort. It is necessary to take into account both heat and moisture transport in and around buildings to predict the hygrothermal behavior of rooms and building walls so as to calculate the energy demands correctly. In this work some benchmark exercises are worked out to see the performance of the heat and moisture transfer model implemented for rooms and porous walls. Finally, numerical results are compared with the measured data for a room exposed to varying outdoor conditions.</itunes:summary>
    </item>
    <item>
      <title>Modelling of absorption of H2O vapor in falling film of lbr aqueous solution in vertical tubes with presence of non-condensables</title>
      <link>http://hdl.handle.net/2117/18010</link>
      <description>Title: Modelling of absorption of H2O vapor in falling film of lbr aqueous solution in vertical tubes with presence of non-condensables
Authors: García-Rivera, Eduardo; Castro González, Jesús; Farnós Baulenas, Joan; Oliva Llena, Asensio
Abstract: One of the main reasons of the discrepancies between theoretical predictions made by models of absorbers of&#xD;
H2O-LiBr absorption chillers when they are compared with experimental results under real conditions is the&#xD;
presence of non-condensables gases. These non-condensables gases are inside the shell of the absorption&#xD;
chiller mainly for two reasons: i) air leakages (Oxygen-Nitrogen); ii) gases produced by corrosion&#xD;
(Hydrogen).&#xD;
A mathematical model of falling film absorption of H2O by LiBr aqueous solutions which considers the&#xD;
influence of non-condensable gases has been implemented. The model is semi-empirical, based on Navier&#xD;
Stokes equations together with energy and mass species simplified under the boundary layer hypotheses.&#xD;
Under such conditions, the differential system of equations in partial derivatives, becomes parabolic and&#xD;
could be solved by means of finite difference method in a step by step procedure. Detailed heat and mass&#xD;
transfer balances are applied at the interface to specify the boundary conditions between liquid and gas&#xD;
phases. In order to calculate gradient of air at the interface, the penetration theory is applied in order to avoid&#xD;
a detailed calculation of the gas phase. Numerically the presence of air in the interface results in a pressure&#xD;
drop and consequently in a reduction in heat and mass transfer rates.</description>
      <pubDate>Wed, 27 Feb 2013 16:26:57 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/18010</guid>
      <dc:date>2013-02-27T16:26:57Z</dc:date>
      <itunes:author>García-Rivera, Eduardo; Castro González, Jesús; Farnós Baulenas, Joan; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>One of the main reasons of the discrepancies between theoretical predictions made by models of absorbers of&#xD;
H2O-LiBr absorption chillers when they are compared with experimental results under real conditions is the&#xD;
presence of non-condensables gases. These non-condensables gases are inside the shell of the absorption&#xD;
chiller mainly for two reasons: i) air leakages (Oxygen-Nitrogen); ii) gases produced by corrosion&#xD;
(Hydrogen).&#xD;
A mathematical model of falling film absorption of H2O by LiBr aqueous solutions which considers the&#xD;
influence of non-condensable gases has been implemented. The model is semi-empirical, based on Navier&#xD;
Stokes equations together with energy and mass species simplified under the boundary layer hypotheses.&#xD;
Under such conditions, the differential system of equations in partial derivatives, becomes parabolic and&#xD;
could be solved by means of finite difference method in a step by step procedure. Detailed heat and mass&#xD;
transfer balances are applied at the interface to specify the boundary conditions between liquid and gas&#xD;
phases. In order to calculate gradient of air at the interface, the penetration theory is applied in order to avoid&#xD;
a detailed calculation of the gas phase. Numerically the presence of air in the interface results in a pressure&#xD;
drop and consequently in a reduction in heat and mass transfer rates.</itunes:summary>
    </item>
    <item>
      <title>Spectrally-consistent regularization modeling of wind farm boundary layers</title>
      <link>http://hdl.handle.net/2117/17948</link>
      <description>Title: Spectrally-consistent regularization modeling of wind farm boundary layers
Authors: Trias Miquel, Francesc Xavier; Folch, David; Gorobets, Andrei; Oliva Llena, Asensio
Abstract: The incompressible Navier-Stokes equations&#xD;
constitute an excellent mathematical modelization of turbulence. Unfortunately, attempts at performing direct simulations are limited to relatively low-Reynolds numbers because of the almost numberless small scales produced by the non-linear&#xD;
convective term. Alternatively, a dynamically less complex formulation is proposed here. Namely, regularizations of the Navier-Stokes equations that preserve the symmetry and conservation properties&#xD;
exactly. To do so, both convective and diffusive term are altered in the same vein. In this way, the convective production of small scales is effectively restrained&#xD;
whereas the modified diffusive term introduces a hyperviscosity effect and consequently enhances the destruction of small scales. In practise, the only&#xD;
additional ingredient is a self-adjoint linear filter whose local filter length is determined from the requirement that vortex-stretching must stop at the smallest&#xD;
grid scale. In the present work, the performance of the above-mentioned recent improvements is assessed through application to homogeneous isotropic turbulence, a turbulent channel flow and a turbulent&#xD;
boundary layer. As a final application, regularization modelling will be applied for large-scale numerical simulation of the atmospheric boundary layer through&#xD;
wind farms.</description>
      <pubDate>Fri, 22 Feb 2013 15:08:48 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17948</guid>
      <dc:date>2013-02-22T15:08:48Z</dc:date>
      <itunes:author>Trias Miquel, Francesc Xavier; Folch, David; Gorobets, Andrei; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The incompressible Navier-Stokes equations&#xD;
constitute an excellent mathematical modelization of turbulence. Unfortunately, attempts at performing direct simulations are limited to relatively low-Reynolds numbers because of the almost numberless small scales produced by the non-linear&#xD;
convective term. Alternatively, a dynamically less complex formulation is proposed here. Namely, regularizations of the Navier-Stokes equations that preserve the symmetry and conservation properties&#xD;
exactly. To do so, both convective and diffusive term are altered in the same vein. In this way, the convective production of small scales is effectively restrained&#xD;
whereas the modified diffusive term introduces a hyperviscosity effect and consequently enhances the destruction of small scales. In practise, the only&#xD;
additional ingredient is a self-adjoint linear filter whose local filter length is determined from the requirement that vortex-stretching must stop at the smallest&#xD;
grid scale. In the present work, the performance of the above-mentioned recent improvements is assessed through application to homogeneous isotropic turbulence, a turbulent channel flow and a turbulent&#xD;
boundary layer. As a final application, regularization modelling will be applied for large-scale numerical simulation of the atmospheric boundary layer through&#xD;
wind farms.</itunes:summary>
    </item>
    <item>
      <title>Numerical simulation of heat transfer and fluid flow in a flat plate solar collector with TIM and ventilation channel</title>
      <link>http://hdl.handle.net/2117/17885</link>
      <description>Title: Numerical simulation of heat transfer and fluid flow in a flat plate solar collector with TIM and ventilation channel
Authors: Kessentini, Hamdi; Capdevila Paramio, Roser; Lehmkuhl Barba, Oriol; Castro González, Jesús; Oliva Llena, Asensio
Abstract: Flat plate solar collector with plastic transparent insulation materials and ventilation channel as overheating protection system inserted between the absorber and the back insulation has been&#xD;
studied numerically. First, a general object-oriented unsteady model of this solar collector is developed and presented. It allows solving, in parallel way, every component separately and interacting with its neighbors to set the boundary conditions in every time step of the simulation. Every component can be simulated using its own mesh and the number of CPUs necessary (depending on the simulation level needed). Second, the numerical simulations of the&#xD;
fluid flow and heat transfer by natural convection in the bottom part (ventilation channel) and the upper part (air gap + TIM) of the collector are done separately. The simulation has taken into account the different operation modes of the channel (opened at high operation temperatures&#xD;
and closed in normal operations). A three dimensional parallel turbulent CFD model based on Large Eddy Simulation is used in the simulations. The obtained numerical results are validated with experimental and benchmark results found in the literature.</description>
      <pubDate>Tue, 19 Feb 2013 15:02:35 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17885</guid>
      <dc:date>2013-02-19T15:02:35Z</dc:date>
      <itunes:author>Kessentini, Hamdi; Capdevila Paramio, Roser; Lehmkuhl Barba, Oriol; Castro González, Jesús; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>Flat plate solar collector with plastic transparent insulation materials and ventilation channel as overheating protection system inserted between the absorber and the back insulation has been&#xD;
studied numerically. First, a general object-oriented unsteady model of this solar collector is developed and presented. It allows solving, in parallel way, every component separately and interacting with its neighbors to set the boundary conditions in every time step of the simulation. Every component can be simulated using its own mesh and the number of CPUs necessary (depending on the simulation level needed). Second, the numerical simulations of the&#xD;
fluid flow and heat transfer by natural convection in the bottom part (ventilation channel) and the upper part (air gap + TIM) of the collector are done separately. The simulation has taken into account the different operation modes of the channel (opened at high operation temperatures&#xD;
and closed in normal operations). A three dimensional parallel turbulent CFD model based on Large Eddy Simulation is used in the simulations. The obtained numerical results are validated with experimental and benchmark results found in the literature.</itunes:summary>
    </item>
    <item>
      <title>Numerical study of the incompressible Richtmyer-Meshkov instability. Interface tracking methods on general meshes</title>
      <link>http://hdl.handle.net/2117/17884</link>
      <description>Title: Numerical study of the incompressible Richtmyer-Meshkov instability. Interface tracking methods on general meshes
Authors: Jofre Cruanyes, Lluís; Balcázar Arciniega, Néstor; Lehmkuhl Barba, Oriol; Castro González, Jesús; Oliva Llena, Asensio
Abstract: The numerical simulation of interfacial and free surface flows is a vast and interesting topic in the areas of engineering and fundamental physics, such as the study of liquid-gas interfaces, formation of droplets,&#xD;
bubbles and sprays, combustion problems with liquid and gas reagents, study of wave motion and others.&#xD;
Many different methods for interface tracking&#xD;
exist, but Volume-of-Fluid and Level-Set methods are two of the most important. The Volume-of-Fluid preserves mass in a natural way but requires large computational resources. On the other hand, the&#xD;
Level-Set is not as accurate and mass conservative as the Volume-of-Fluid but is a faster way to track&#xD;
interfaces, representing them by the middle contour of&#xD;
a signed distance function.&#xD;
The objective of this work is to analyze the&#xD;
advantatges and drawbacks of the Volume-of-Fluid&#xD;
and Level-Set methods by solving the incompressible&#xD;
two-liquid Richtmyer-Meshkov instability and to&#xD;
compare the results to experimental data.</description>
      <pubDate>Tue, 19 Feb 2013 14:33:54 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17884</guid>
      <dc:date>2013-02-19T14:33:54Z</dc:date>
      <itunes:author>Jofre Cruanyes, Lluís; Balcázar Arciniega, Néstor; Lehmkuhl Barba, Oriol; Castro González, Jesús; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The numerical simulation of interfacial and free surface flows is a vast and interesting topic in the areas of engineering and fundamental physics, such as the study of liquid-gas interfaces, formation of droplets,&#xD;
bubbles and sprays, combustion problems with liquid and gas reagents, study of wave motion and others.&#xD;
Many different methods for interface tracking&#xD;
exist, but Volume-of-Fluid and Level-Set methods are two of the most important. The Volume-of-Fluid preserves mass in a natural way but requires large computational resources. On the other hand, the&#xD;
Level-Set is not as accurate and mass conservative as the Volume-of-Fluid but is a faster way to track&#xD;
interfaces, representing them by the middle contour of&#xD;
a signed distance function.&#xD;
The objective of this work is to analyze the&#xD;
advantatges and drawbacks of the Volume-of-Fluid&#xD;
and Level-Set methods by solving the incompressible&#xD;
two-liquid Richtmyer-Meshkov instability and to&#xD;
compare the results to experimental data.</itunes:summary>
    </item>
    <item>
      <title>A filtered kinetic energy preserving finite volumes scheme for compressible flows</title>
      <link>http://hdl.handle.net/2117/17883</link>
      <description>Title: A filtered kinetic energy preserving finite volumes scheme for compressible flows
Authors: Baez Vidal, Aleix; Lehmkuhl Barba, Oriol; Pérez Segarra, Carlos David; Oliva Llena, Asensio
Abstract: The Kinetic Energy Preserving Scheme (KEP)&#xD;
for compressible flows has been shown to solve 1-D shock waves without smearing them. The method does not add numerical diffusion to solutions but, as a counterpart, it needs very dense meshes in order to be Local Variations Diminishing (LVD) and&#xD;
stable. For 2-D and 3-D geometries, the method needs unaffordable meshes. A Filtered Kinetic Energy Preserving Method (FKEP) that partially solves this issue is presented in this document. The method filters&#xD;
the solution obtained by a KEP at each time step. It is shown that the use of filters does not significantly change the low frequencies of the motion while it&#xD;
enables the use of much coarser meshes.FKEP is tested on the 1-D shock tube.</description>
      <pubDate>Tue, 19 Feb 2013 14:19:03 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17883</guid>
      <dc:date>2013-02-19T14:19:03Z</dc:date>
      <itunes:author>Baez Vidal, Aleix; Lehmkuhl Barba, Oriol; Pérez Segarra, Carlos David; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The Kinetic Energy Preserving Scheme (KEP)&#xD;
for compressible flows has been shown to solve 1-D shock waves without smearing them. The method does not add numerical diffusion to solutions but, as a counterpart, it needs very dense meshes in order to be Local Variations Diminishing (LVD) and&#xD;
stable. For 2-D and 3-D geometries, the method needs unaffordable meshes. A Filtered Kinetic Energy Preserving Method (FKEP) that partially solves this issue is presented in this document. The method filters&#xD;
the solution obtained by a KEP at each time step. It is shown that the use of filters does not significantly change the low frequencies of the motion while it&#xD;
enables the use of much coarser meshes.FKEP is tested on the 1-D shock tube.</itunes:summary>
    </item>
    <item>
      <title>Solid-liquid phase change with turbulent flow</title>
      <link>http://hdl.handle.net/2117/17861</link>
      <description>Title: Solid-liquid phase change with turbulent flow
Authors: Galione, Pedro; Rigola Serrano, Joaquim; Castro González, Jesús; Rodríguez Pérez, Ivette María
Abstract: The present paper describes a numerical simulation of the solid-liquid phase change Computational&#xD;
Fluid Dynamics and Heat Transfer (CFD&amp;HT) model developed in order to account for natural&#xD;
convection inside Phase Change Materials (PCMs) taking into account turbulent effects.</description>
      <pubDate>Mon, 18 Feb 2013 16:24:36 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17861</guid>
      <dc:date>2013-02-18T16:24:36Z</dc:date>
      <itunes:author>Galione, Pedro; Rigola Serrano, Joaquim; Castro González, Jesús; Rodríguez Pérez, Ivette María</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The present paper describes a numerical simulation of the solid-liquid phase change Computational&#xD;
Fluid Dynamics and Heat Transfer (CFD&amp;HT) model developed in order to account for natural&#xD;
convection inside Phase Change Materials (PCMs) taking into account turbulent effects.</itunes:summary>
    </item>
    <item>
      <title>Detailed numerical model for the resolution of molten salt storage tanks for CSP plants</title>
      <link>http://hdl.handle.net/2117/17441</link>
      <description>Title: Detailed numerical model for the resolution of molten salt storage tanks for CSP plants
Authors: Pérez Segarra, Carlos David; Rodríguez Pérez, Ivette María; Oliva Llena, Asensio; Torras Ortíz, Santiago; Lehmkuhl Barba, Oriol
Abstract: Considering the state-of-the-art in TES technologies, two-tank indirect system using molten salt is the most widespread within CSP plants. However, current techniques for design and optimization, as well as, for assessing the behaviour of these systems are mainly based on not-to-scale costly&#xD;
experimental set-ups. In this paper, a detailed numerical methodology modelling molten salt thermal storage tanks is presented. This methodology considers the transient behaviour of the molten-salt fluid, the gas ullage, the molten-salt free surface, the tank walls and insulation, different material in the foundation, radiation exchange between the salt and the tank walls in the ullage, the passive cooling in the foundation is proposed. Results for different configuration which allows an optimal design of the tank walls, insulation materials and tank foundations are presented.</description>
      <pubDate>Mon, 21 Jan 2013 14:51:05 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17441</guid>
      <dc:date>2013-01-21T14:51:05Z</dc:date>
      <itunes:author>Pérez Segarra, Carlos David; Rodríguez Pérez, Ivette María; Oliva Llena, Asensio; Torras Ortíz, Santiago; Lehmkuhl Barba, Oriol</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>Considering the state-of-the-art in TES technologies, two-tank indirect system using molten salt is the most widespread within CSP plants. However, current techniques for design and optimization, as well as, for assessing the behaviour of these systems are mainly based on not-to-scale costly&#xD;
experimental set-ups. In this paper, a detailed numerical methodology modelling molten salt thermal storage tanks is presented. This methodology considers the transient behaviour of the molten-salt fluid, the gas ullage, the molten-salt free surface, the tank walls and insulation, different material in the foundation, radiation exchange between the salt and the tank walls in the ullage, the passive cooling in the foundation is proposed. Results for different configuration which allows an optimal design of the tank walls, insulation materials and tank foundations are presented.</itunes:summary>
    </item>
    <item>
      <title>Large-eddy simulations of fluid flow and heat transfer around a parabolic trough solar collector</title>
      <link>http://hdl.handle.net/2117/17439</link>
      <description>Title: Large-eddy simulations of fluid flow and heat transfer around a parabolic trough solar collector
Authors: Amine Hachicha, Ahmed; Rodríguez Pérez, Ivette María; Oliva Llena, Asensio
Abstract: This study reports on numerical simulations of a parabolic trough solar collector to predict the aerodynamic behaviour and the convection heat transfer from the heat collector element. In the study, the variation of fluid flow with different angles of attack has been taken into account.&#xD;
Calculations are performed using Large Eddy Simulations with a Variational Multiscale (VMS)approach for modelling the sub-grid scale stress tensor. The governing equations are discretised on a collocated unstructured grid arrangement by means of second-order spectro-consistent schemes.&#xD;
The numerical model is validated first with a cross flow around a horizontal cylinder. After that,aerodynamic coefficients at different angles of attack or pitch angles are calculated and compared to wind-tunnel experiments. It has been shown that, the orientation of the solar collector plays an&#xD;
important role in evaluating the aerodynamic performance and structural design criteria of the collector.</description>
      <pubDate>Mon, 21 Jan 2013 14:31:43 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17439</guid>
      <dc:date>2013-01-21T14:31:43Z</dc:date>
      <itunes:author>Amine Hachicha, Ahmed; Rodríguez Pérez, Ivette María; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>This study reports on numerical simulations of a parabolic trough solar collector to predict the aerodynamic behaviour and the convection heat transfer from the heat collector element. In the study, the variation of fluid flow with different angles of attack has been taken into account.&#xD;
Calculations are performed using Large Eddy Simulations with a Variational Multiscale (VMS)approach for modelling the sub-grid scale stress tensor. The governing equations are discretised on a collocated unstructured grid arrangement by means of second-order spectro-consistent schemes.&#xD;
The numerical model is validated first with a cross flow around a horizontal cylinder. After that,aerodynamic coefficients at different angles of attack or pitch angles are calculated and compared to wind-tunnel experiments. It has been shown that, the orientation of the solar collector plays an&#xD;
important role in evaluating the aerodynamic performance and structural design criteria of the collector.</itunes:summary>
    </item>
    <item>
      <title>Spectrally-consistent regularization modeling of turbulent natural convection flows</title>
      <link>http://hdl.handle.net/2117/17430</link>
      <description>Title: Spectrally-consistent regularization modeling of turbulent natural convection flows
Authors: Trias Miquel, Francesc Xavier; Verstappen, R.W.C.P.; Gorobets, Andrei; Oliva Llena, Asensio
Abstract: The incompressible Navier-Stokes equations constitute an excellent mathematical&#xD;
modelization of turbulence. Unfortunately, attempts at performing direct simulations are&#xD;
limited to relatively low-Reynolds numbers because of the almost numberless small scales&#xD;
produced by the non-linear convective term. Alternatively, a dynamically less complex&#xD;
formulation is proposed here. Namely, regularizations of the Navier-Stokes equations that preserve the symmetry and conservation properties exactly. To do so, both convective and diffusive terms are altered in the same vein. In this way, the convective production of small scales&#xD;
is effectively restrained whereas the modified diffusive term introduces a hyperviscosity effect and consequently enhances the destruction of small scales. In practice, the only additional ingredient&#xD;
is a self-adjoint linear filter whose local filter length is determined from the requirement that vortex-stretching must stop at the smallest grid scale. In the present work, the performance of the above-mentioned recent improvements is assessed through application to turbulent natural&#xD;
convection flows by means of comparison with DNS reference data.</description>
      <pubDate>Fri, 18 Jan 2013 16:04:42 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17430</guid>
      <dc:date>2013-01-18T16:04:42Z</dc:date>
      <itunes:author>Trias Miquel, Francesc Xavier; Verstappen, R.W.C.P.; Gorobets, Andrei; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The incompressible Navier-Stokes equations constitute an excellent mathematical&#xD;
modelization of turbulence. Unfortunately, attempts at performing direct simulations are&#xD;
limited to relatively low-Reynolds numbers because of the almost numberless small scales&#xD;
produced by the non-linear convective term. Alternatively, a dynamically less complex&#xD;
formulation is proposed here. Namely, regularizations of the Navier-Stokes equations that preserve the symmetry and conservation properties exactly. To do so, both convective and diffusive terms are altered in the same vein. In this way, the convective production of small scales&#xD;
is effectively restrained whereas the modified diffusive term introduces a hyperviscosity effect and consequently enhances the destruction of small scales. In practice, the only additional ingredient&#xD;
is a self-adjoint linear filter whose local filter length is determined from the requirement that vortex-stretching must stop at the smallest grid scale. In the present work, the performance of the above-mentioned recent improvements is assessed through application to turbulent natural&#xD;
convection flows by means of comparison with DNS reference data.</itunes:summary>
    </item>
    <item>
      <title>Spectrally-consistent regularization modeling at very high Rayleigh numbers</title>
      <link>http://hdl.handle.net/2117/17429</link>
      <description>Title: Spectrally-consistent regularization modeling at very high Rayleigh numbers
Authors: Trias Miquel, Francesc Xavier; Gorobets, Andrei; Verstappen, R.W.C.P.; Oliva Llena, Asensio
Abstract: The incompressible Navier-Stokes equations constitute an excellent mathematical modelization of turbulence. Unfortunately, attempts at performing direct simulations are limited to relatively low-Rayleigh numbers because of the almost numberless small scales produced by the non-linear convective term. Alternatively, a dynamically less complex formulation is proposed here. Namely, regularizations of&#xD;
the Navier-Stokes equations that preserve the symmetry and conservation properties exactly. To do so, both convective and diffusive term are altered in the same vein. In this way, the convective production of small scales is effectively restrained whereas the modified diffusive term introduces a hyperviscosity effect and&#xD;
consequently enhances the destruction of small scales. In practice, the only additional ingredient is a selfadjoint&#xD;
linear filter whose local filter length is determined from the requirement that vortex-stretching must stop at the smallest grid scale. The performance of the novel regularization modeling approach is assessed&#xD;
through application to turbulent natural convection flows at very high Rayleigh numbers</description>
      <pubDate>Fri, 18 Jan 2013 15:42:27 GMT</pubDate>
      <guid isPermaLink="false">http://hdl.handle.net/2117/17429</guid>
      <dc:date>2013-01-18T15:42:27Z</dc:date>
      <itunes:author>Trias Miquel, Francesc Xavier; Gorobets, Andrei; Verstappen, R.W.C.P.; Oliva Llena, Asensio</itunes:author>
      <itunes:explicit>no</itunes:explicit>
      <itunes:keywords />
      <itunes:summary>The incompressible Navier-Stokes equations constitute an excellent mathematical modelization of turbulence. Unfortunately, attempts at performing direct simulations are limited to relatively low-Rayleigh numbers because of the almost numberless small scales produced by the non-linear convective term. Alternatively, a dynamically less complex formulation is proposed here. Namely, regularizations of&#xD;
the Navier-Stokes equations that preserve the symmetry and conservation properties exactly. To do so, both convective and diffusive term are altered in the same vein. In this way, the convective production of small scales is effectively restrained whereas the modified diffusive term introduces a hyperviscosity effect and&#xD;
consequently enhances the destruction of small scales. In practice, the only additional ingredient is a selfadjoint&#xD;
linear filter whose local filter length is determined from the requirement that vortex-stretching must stop at the smallest grid scale. The performance of the novel regularization modeling approach is assessed&#xD;
through application to turbulent natural convection flows at very high Rayleigh numbers</itunes:summary>
    </item>
  </channel>
</rss>

