School of Mechanical Aerospace and Civil Engineering The University of Manchester Centre for Modelling and Simulation Pre launch Meeting Fluids Group: Summaries ...

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CFD TM Meeting. Date : May 28th 2008 Venue : George Begg, B8. Participants : All MACE students, researchers academics interested in collaborative developments ...

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Neil: Hybrid numerics case. currently shows hybrid scheme is same as centered. need to test on unstructured mesh, or mesh where there are distinct regions of RANS ...

progress 23 3.ppt: progress 23 3.ppt

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Weekly Group Meeting (GB C21) The weekly meeting takes place every tuesday, from the 27th of May onwards, in the Aquarium. Each time there will be a Chairman and ...

Some new results on the bypass transition over a plat flate : Cf flatplate.png:

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Date 03 June 2008 Location C012 Geoge Begg (Acquarium) Attendees Stefano Ulka Flavien Juan Alistair Yacine Claire ...

Date 10 June 2008 Location C021 Geoge Begg (library) Attendees Stefano Ulka Flavien Juan Alistair Yacine Claire ...

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Summaries of Current Ph.D. Research Projects Location : GB C21 Time : Afternoon Session (13:30 15:30). Subject : Overview of the current Ph.D. Projects ...

List of seminars

As recently remarked by Sagaut and Deck 1 hybrid RANS/LES techniques are the main strategy to reduce computational cost compared to LES when attached boundary layers ...

It is the purpose of this study to evaluate the characteristics of the generation and propagation of compressible vortex rings in a shock tube where the physical properties ...

Jarrin et al. (2009) developed the Synthetic Eddy Method (SEM) as a quasi particle based method to generate synthetic turbulence conditions for embedded LES. The method ...

Interest in the development of flapping wing air vehicles has prompted a significant amount of research on the kinematics and aerodynamics of flapping flight in nature ...

The reliable computation of buoyant flows is important in a number of engineering sectors, including the nuclear one. Here, turbulent natural convection of air in ...

Inlet Barrier Filter systems (IBF) are an essential piece of hardware in the operation of helicopters to and from unprepared landing sites. They are installed ahead ...

SPH is a relatively new, rapidly evolving Lagrangian meshless method that is currently being applied in a large variety of cases, ranging from astrophysics to nuclear ...

The subject of generating oscillatory motion in fluids operating without moving components is relatively less well known. However, the idea is not new – first oscillators ...

The single dielectric barrier discharge plasma actuators have shown their positive effectiveness amongst the other active flow control methods with the advantageous ...

The optimisation of helicopter design and aerodynamic performance has traditionally been achieved through experimental studies and empirical calculations, but over ...

Hypersonic flight within the atmosphere is of current interest, both military and civilian. Even though it has been become more reachable with the advent of new technologies ...

Experiments conducted in the Advanced Gas cooled Reactor (AGRs) design stages indicate a three dimensional flow swirl present in the in line tube bank section of certain ...

In many experimental and numerical problems, the physical behaviours of a system should be quantified and a configuration for obtaining the optimal condition should ...

Quadrotor helicopters have emerged as a design alternative to conventional helicopter designs for UAV in the range of a few kg. They are envisaged for operations in ...

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Internal Seminar Series 2011, , School of MACE, The University of Manchester Files: Abstract: Presentation: Abstract " hideimgleft ""}% ...

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Open Source Software for engineers Here is a list of the open source software that I am aware of. Please feel free to add any program that you consider relevant. ...

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PG10Poster performance of two kt kl w models in a separation induced transition test case.ppt: Poster for the PGR Conference 2010

An update of the work done on the Valeo Aerofoil test case for Fred Mendonca of CD adapco, after discussions at the STAR European Conference. The power point goes ...

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Study of the effects of non conformal mesh refinements using the Taylor Green vortices.

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Any additional information or links can be added here. KNOO Meeting HMS Sultan July 2007.ppt: KNOO Meeting HMS Sultan July 2007.ppt

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Temporary uploaded manual of star ccm

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Tyndall project presentation

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This presentation includes a rough introduction of transformer structure, transformer thermal solutions and current industry progress about the transformer thermal ...

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Any additional information or links can be added here. France Japan joint Seminar on Thermal fatigue, 5th to 6th October 2009, Tokyo, Japan Tokyo meeting knoo ...

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Presentation on Natural Convection in Square Cavity, checking for convergence errors 17 November 2009

Presentation for the SPH meeting 23/11/2009

Rotation and curvature greatly affect a turbulent motion. Basic effects of rotation on turbulence are non linear : two points correlations are modified in such a way ...

Rotation and curvature greatly affect a turbulent motion. Basic effects of rotation on turbulence are non linear : two points correlations are modified in such a way ...

Rotation and curvature greatly affect a turbulent motion. Basic effects of rotation on turbulence are non linear : two points correlations are modified in such a way ...

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Rotation and curvature greatly affect a turbulent motion. Basic effects of rotation on turbulence are non linear : two points correlations are modified in such a way ...

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Presentation: Download

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Presentation for the UniMan weekly meeting that should be reported to the ATAAC meeting in Berlin (11/2010)

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This presentation was given as a brief introduction to memory hierarchies and cache use.

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Presentation for the CodeSaturne user meeting Paris, Dec. 2010

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PDF and PPT versions available 04 REVELL.pdf 04 REVELL.ppt This was presented in July 2011 as an invited lecture at the EDF Research event "R D industrielle ...

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Last Published Publisher DavidMonfort Date 2011 09 15 09:31 {PublishContrib}{Dir} /home/httpd/twiki/pub/publish/ {PublishContrib}{URL} http://cfd.mace.manchester ...

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Any additional information or links can be added here. Awarded as the Best Presentation in FLOW PHYSICS COMBUSTION section.

Analysis of Launder Sharma and k g %$(g \ \alpha \ 1/\omega)$% for a transitional separation bubble using DNS data. A Wilcox transition modification was found to ...

The equations of the most common RANS models are simplified in the near wall region and in the log layer, in the very simple case of a 1D channel flow .

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Chabard HMFF4tomorrows energy 20090616 final fa Preprint.pdf: Preprint version 2009 06 16 website:  www.thmt 09.org draft ppt 00a THMT JPC DL 09 09 09 Introduction ...

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Non structured LES of a complex geometry (a simplified car body) at Reynolds number %$4.29 \times 10^6$% PDF

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The %$k \epsilon$% models tend to have some difficulty in modelling the reduction in turbulence intensity due to the skewing process: The modelling of a term ...

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DOI: 10.1007/978 3 540 77815 8 ISBN 978 3 540 77813 4 http://www.springerlink.com/content/978 3 540 77813 4 Advances in Hybrid RANS LES Modelling Papers contributed ...

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http://dx.doi.org/doi:10.1016/j.jcp.2008.06.005 Received 21 December 2006; revised 29 January 2008; accepted 9 June 2008. Available online 19 June 2008.

http://dx.doi.org/doi:10.1016/j.ijheatfluidflow.2008.02.010 Received 28 May 2007; revised 15 February 2008; accepted 18 February 2008. Available online 8 April ...

http://dx.doi.org/doi:10.1016/j.ijmultiphaseflow.2008.04.002 Received 30 September 2007; revised 24 April 2008. Available online 10 May 2008.

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ISBN: 978 1 4020 8577 2. Online version available at http://www.springerlink.com/content/978 1 4020 8577 2 Paper Submitted : 1 October 1, 2007 Online Publication Date ...

Extended version submitted to IJHFF "special issue on selected papers from ETMM7 2008 conference" Jarrin HFF 2008.pdf: Preprint of Jarrin HFF 2008.pdf draft submitted ...

DOI 10.1007/978 90 481 3652 0 60 Download

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Any additional information or links can be added here.Received 1 July 2008; revised 7 September 2008; accepted 8 September 2008. Available online 10 October 2008 ...

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Any additional information or links can be added here. First Year Progression Report has been submitted and examined (September 2007).

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Any additional information or links can be added here. I. J. Heat Fluid Flow, Vol 28, Issue 4, August 2007, pp 561 574Afgan I., Moulinec C., Prosser R., Laurence ...

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DOI:10.1002/fld.1719 http://doi.wiley.com/10.1002/fld.1719

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A linearised turbulent production in the k epsilon model., Guimet V., Laurence D., 5th Engineering Turbulence Modelling and Measurements. Mallorca, Spain. 16 18th ...

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Any additional information or links can be added here. An Overset Grid Strategy for Aeroacoustics and Aeroelasticity of Moving Bodies

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This paper is available online by following link:

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first year report Ali Omranian.pdf: first year report Ali Omranian.pdf

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Attachment to the pubblication: Pre print copy ICAPP'10: Download Animations: 7 pins configuration, H/D 21, %$Re 5000$%, %$R {ij}$% turbulence ...

Set ALLOTOPICVIEW RobertoLotto,BenedicteRogers,DominiqueLaurence

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Link to the paper

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http://www.springerlink.com/content/t383079621247464/

http://www.ctresources.info/ccp/paper.html?id 5179 doi 10.4203/ccp.90.2

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Download

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Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 2010, Volume 110/2010, 385 391, DOI: 10.1007/978 3 642 14139 3 47

This paper was first archived as an internal EDF R D report with reference: H I83 2011 00185 EN, (same authors and title), (issued) 25 Jan 2011, in Press ...

Any additional information or links can be added here. Presented at 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ...

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This is the thesis of the MPhil I passed in Manchester.

This is the thesis I passed in Manchester in 2010. Thesis Olivier COZZI.pdf: This is the pdf version of the thesis.

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Report2.pdf: This is my second year report

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THMT09 poster a0 2.pdf: The poster for the THMT conference thmt 09CT.pdf: The short paper for the THMT conference

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Full paper available via Springer here: http://www.springerlink.com/content/g206763436175133/ Earlier draft version here: Laurence Uribe Utyu2004 V2F.pdf:  (Laurence ...

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doi 10.1007/978 1 4020 9898 7 6 Braza, M. and Houringan, K. editors IUTAM Bookseries, Springer

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.

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Any additional information or links can be added here. EDT PhD Dalila AMMOUR FINAL.pdf: EDT PhD Dalila AMMOUR FINAL.pdf

A modified eddy viscosity model is proposed to model the misalignment between stress and strain fields for variable density flows. The stress strain misalignment is ...

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Download conference paper draft here: Hanjalic Laurence Popovac Uribe ETMM6draft05 2005.pdf

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LES or even DNS computation on complex geometries need to use unstructured mesh, in order to keep the mesh size reasonable. This type of grids raises some numerical ...

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This paper is available directly from the CTR website, at address

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Summary A new eddy viscosity model is proposed to include stress strain lag effects in the modelling of unsteady mean flows. A transport equation for the lag parameter ...

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The thesis is available as a pdf: Phd Parham Momeni.pdf (file size around 30MB)

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Journal and Conference Publications " hideimgleft "" suffix "" firststart "show" remember "on"}% %SEARCH{" " hideimgleft "" suffix "" firststart "show" remember "on ...

Fuel rod bundle arranged into a triangular array A fuel rod bundle arranged in a triangular array is investigated using well resolved LES. When the pitch to diameter ...

Developments of the proposed model : BL %$\overline{v^2}/k$% model A new but well validated and truly robust version of an elliptic blending low Reynolds number eddy ...

1 Mixed Convection flows in vertical heated pipes It has been sought to examine a number of advanced, and distinct, Eddy Viscosity RANS Models (EVMs) against experimental ...

1 Introduction As the UK's fleet of Advanced Gas cooled Reactors (AGRs) approach the end of their operational lives, ageing effects must be remediated for a number ...

Transition prediction with popular RANS models The type of transition we are concerned with here is bypass transition (induced by external flow turbulence), which ...

Introduction Why Delayed Detached Eddy Simulation (DDES)? Hybrid RANS LES models have become a viable alternative to RANS and LES methods for solving massively separated ...

Buoyancy flow in square cavity has been taken as a first test case. Effect of three different kind of grids with varying cell densities have been studied to see their ...

\usepackage{graphicx} \usepackage{subfigure} \usepackage dvips {graphics} Dealing with wall boundary conditions is one of the most challenging parts of the SPH ...

Abstract This research is concerned with the wing of the C Class catamaran of Team Invictus, see figure 1. The current wing is a reverse engineered design of a previous ...

GPU Technology GPUs differ from traditional CPUs by having far more 'processing cores' at the expense of having less cache memory. Cache is very fast (and therefore ...

The project started in October 2009 with the supervision of Dr. Alistair Revell and Dr. Tim Craft. To date the following steps has been done: Review of the literature ...

STEP 1 Introduction SEM method, created and implemented by N. Jarrin (2009), is one way used to create inlet conditions for a LES directly from a RANS solution ...

Introduction Fires are unwanted and uncontrolled combustion events that occur everyday around the world and cause immense material damages and loss of life. For example ...

Non isothermal turbulent convection flows are encountered in nature and in many engineering applications involving either buoyancy or thermal stratification. Our focus ...

1.Asymmetric Diffuser (Code Saturne v1.3.3): Different turbulence models are tested for their prediction of the separation region of the flow. 2.Shock Tube (OpenFoam ...

As this PhD started only recently no significant and non preliminary results could be produced yet.

Currently simulations are in progress using different existing scalar dissipation models. These scalar dissipation models vary in complexity and require either algebraic ...

State of the art Grojans and Menter (1998) have developed the "scalable wall function" that allow one to use any mesh preserving the precision of the high Reynolds ...

Research Summary Details Form Name Type Size Values Tooltip message Attributes Name text 80 Name of the researcher Title ...

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Research Tools Here are some tools that research students might find useful. Please feel free to add your comments, scripts, examples etc. For a list of all Open Source ...

RuggeroPoletto 2010 04 30

Saturne Validation page The purpose of this page is to create a pdf report on all the cases that are on the wiki. It uses the plugin : http://cfd.mace.manchester.ac ...

Name NONE

Additional information (links, pictures, etc.) The initial choice of the computational domain is made by examining experimental two point correlations. The computational ...

Aditional information: To run the case just copy the FORTRAN files and modify the lance script accordingly: fotrans v1.3.2.tar: Fortrans and lance script used ...

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RANS RESULTS The results are in good agreement with the previous version (see figure 1). In figures 2 and 3 the results for velocity and kinetic energy with the high ...

Additional information (links, pictures, etc.) This is a challenging test case for wall function approaches. The results are sensitive ...

2dcyl lowRe.unv.gz: 2dcyl lowRe.unv.gz 2dcyl LRE fine.unv.gz: 2dcyl LRE fine.unv.gz 2dcyl.unv.gz: 2dcyl.unv.gz

Additional information (links, pictures, etc.) The experiment has been done with a leading edge slot that covers the entire span of the aerofoil. The total span of ...

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Case definition (additional information) Steady state %$Re 2650$% (based on radius) %$\Rightarrow Re \tau 180$% GRashof number %$Gr \frac{g \beta ...

LS CONVERT.zip: LS CONVERT.zip

CI CONVERT.zip: CI CONVERT.zip

Suga CONVERT.zip: Suga CONVERT.zip

DNS You et al 2003.zip: DNS You et al 2003.zip TWiki 4.1.2, Sat, 03 Mar 2007, build 13046 TWiki 4.1.2, Sat, 03 Mar 2007, build 13046 TWiki 4.1.2, Sat, 03 Mar 2007 ...

LES StarCD.zip: LES StarCD.zip

ManV2F Saturne.zip: ManV2F Saturne.zip

Std k eps StarCD.zip: Std k eps StarCD.zip

k omg StarCD.zip: k omg StarCD.zip

Additional information (links, pictures, etc.) tube bundle description:

Additional information (links, pictures, etc.)

Discussion. Similarly to the V1.3.0 validation, vertical profile of horizontal velocity is the same for all convection schemes of order 2. The upwind scheme yields ...

Geometrical features Length of the field :%$L 38m$% Width of the field :%$h 12m$% Diameter of the cylinder :%$d 1.5m$% Position of the%$C$%center ...

Additional information (links, pictures, etc.) Part of the 15 ERCOFTAC workshop at: Diffuser geometry: Experimental results visualization ...

Additional information (links, pictures, etc.) Ercoftac c13.2 UoM.tar.bz2: Results Velocity profiles at z/H 2: Velocity profiles at z/H 2 (second ...

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Additional information (links, pictures, etc.)

Additional information (links, pictures, etc.) To run the case using Code Saturne : Fortran subroutines to be added in the FORT directory: usclim.F, ushist ...

Data available The following data is available for comparison 1 : Pressure coefficient %$Cp (p px) / (0.5 \rho U b^2)$% along the inclined bottom wall and ...

Additional information (links, pictures, etc.) Saturne user subroutines to run the inlet case: inccas.h, usclim.F, ushist.F, usini1.F, usiniv.F, usproj ...

Additional information (links, pictures, etc.) profiles at x/h 6: profiles at x/h 3: profiles at x/h 14: profiles ...

Additional information (links, pictures, etc.) figures 1 5 show the results of the current version compared to the previous. All profiles are in good agreement showing ...

Additional information (links, pictures, etc.) Simulation Details: The simulation was performed over a grid of approximately 5M nodes, covering a spanwise direction ...

Case Setup In this tar file you will find the FORTRANS and the lance script necessary to setup the case under version 1.3.2. fort SST.tar.gz: FORTRANS to set ...

Additional information (links, pictures, etc.) cavity sst.tar.gz: SST results Vertical VelocityTemperature Profiles (profiles are at y/H 0.05, 10, 30 ...

Discussion Simulations consisted in comparing three kinds of turbulent models and the effects of the wall function parameter (ideuch) in the models. Seven simulations ...

Additional information (links, pictures, etc.) Snapshots of instantaneous temperature distribution from different T junction configurations (see references cited above ...

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Additional information (links, pictures, etc.) Tjunction.zip: a sample grid FORT 1.3.2.zip: fortran source code to run the case Data CASE1 Straight ...

Additional information (links, pictures, etc.) The case was considered at the 4th ERCOFTAC/IAHR Workshop on Refined Flow Modelling, held at Karlsruhe in 1995. The ...

Additional information (links, pictures, etc.) The analytical inlet profiles are given by: %$ U u^ (\frac{log(1 0.4y^ )}{0.42} 7.8(1 \exp( y^ /11) y^ \exp ...

Discussion The inlet profiles are imposed using the following equations: %$ U u^ (\frac{log(1 0.4y^ )}{0.42} 7.8(1 \exp( y^ /11) y^ \exp( 0.33y^ /11) )$% %$ k ...

Additional information (links, pictures, etc.) pk 12 half merged.unv: P/k 12 1s fine but only one rib. Gaps fixed

Discussion

Discussion As no modification has been done in the current version of the code (compared to 1.3 version), no mesh sensitivity has been done. The reader can refer to ...

Discussion Comparison of the models Figures (1), (2) and (3) compares the different models %$k \varepsilon$% with and without linear production and %$R {ij} \varepsilon ...

Additional information (links, pictures, etc.) In these calculation, we notice that the size of the cathode region is very important data but it is not well known ...

Additional information (links, pictures, etc.) On the following figures, the comparison between 1.3 and 2.0 models gives identical results, in agreement with the Gaussian ...

Discussion The following figures show two temperature profiles obtained on two location. As a general conclusion, the present results are all similar and close to ...

Additional information (links, pictures, etc.) Smooth rough velocity: Rough smooth velocity: Smooth rough surface stress: Rough smooth ...

Additional information (links, pictures, etc.) Smooth rough velocity: br / img width "1200" alt "USR 09171748 6.png" src "/USR 09210928 6.png" height "900" ...

Additional information (links, pictures, etc.) This test case is dedicated to the verification of the rough law of the wall, with different roughness (in meters). ...

Additional information (links, pictures, etc.) Using options extrag(ipr(iphas)) 1 leads to non convergence of version 2.0 beta2 on this case. For k variables ...

Analysis of the numerical results The analytic results available are given as different profiles for the radiative source term (profiles inside the domain) and the ...

Discussion The simulations have been run on all the production servers at EDF (at the time being), i.e. Calibre 5 and CCRT (Platine). The following graphs show the ...

Additional information (links, pictures, etc.) Figure 1 Test geometry Domain characteristics section width : %$150 mm$% section height : %$350 mm$% ...

Additional information (links, pictures, etc.) Particle volume fraction Particle vertical velocity (average) Particle vertical velocity (fluctuating ...

Additional information (links, pictures, etc.) The simulations show that we recover results of the previous version 1.3.1 from a qualitative and analytical point of ...

Additional information (links, pictures, etc.) Figure 1 Domain geometry Particles parameters As flow parameters, particles characteristics are taken from 1 ...

Additional information (links, pictures, etc.) Two discrepancies between versions 1.3 and 2.0 can be noted in the following results. The first one concerns the inlet ...

Additional information (links, pictures, etc.) Though an error is present in the calculation of the displacement, this does not impair the results presented herebelow ...

Additional information (links, pictures, etc.) Geometry 3D Co flow Mesh file mailhexa.des: mailhexa.des

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Boundary conditions Fuel inlet: Total flowrate: %$2.62609\times10^{ 4}kg.s^{ 1}$% Temperature : %$436 K$% Mixing Rate : %$1$% Air inlet: Total flowrate ...

Here below are presented the results for the streamwise velocity on the different sections. We can here see that the results between both versions are quite similar ...

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Physical forcing Radiative forcing The short wave and long wave radiative forcing were taken into account by adding additional radiative source terms (ustssn.f90 ...

Boundary conditions The single inlet parameters are given in the following table 1: Inlet Value Total coal mass flow 450 kg/h Total primary air ...

In the following figures 4 to 7 the axial and tangential velocities profiles,respectively, the gas temperature, and the volumetric concentrations of %$CO 2$% and ...

3D visualization mean velocities and turbulent kinetic energy fields: Figure 9: Mean streamwise and spanwise velocity fields and mean turbulent kinetic energy ...

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FlavienBillard 2010 04 01

FlavienBillard 2010 04 01

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FlavienBillard 2010 04 01

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First year Report, submittted in September 2007

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