Combining the strengths of UMIST and The Victoria University of Manchester Laminar Kinetic Energy Models in Code_Saturne Presented by Clare Turner.

Slides:



Advertisements
Similar presentations
Introduction to Computational Fluid Dynamics
Advertisements

School of Mechanical, Aerospace & Civil Engineering Postgraduate Research Conference, PGR-MACE10 Performance of two k T -k L -ω models in a separation-induced.
Instructor: André Bakker
Outline Overview of Pipe Flow CFD Process ANSYS Workbench
Svetlana Marmutova Laminar flow simulation around circular cylinder 11 of March 2013, Espoo Faculty of Technology.
Jet Engine Design Idealized air-standard Brayton cycle
Analysis of the Droplet Size Reduction in a pMDI Due to the Addition of a Turbulence Generating Nozzle by Michael P. Medlar Dr. Risa Robinson.
Review of the Valeo-CD Aerofoil Tests Clare Turner.
..perhaps the hardest place to use Bernoulli’s equation (so don’t)
Advanced CFD Analysis of Aerodynamics Using CFX
Evan Greer, Mentor: Dr. Marcelo Kobayashi, HARP REU Program August 2, 2012 Contact: globalwindgroup.com.
Experimental and Numerical Study of the Effect of Geometric Parameters on Liquid Single-Phase Pressure Drop in Micro- Scale Pin-Fin Arrays Valerie Pezzullo,
Wind Chill Factor Regie Hyppolite and Justin Hyatt.
Combining the strengths of UMIST and The Victoria University of Manchester Aspects of Transitional flow for External Applications A review presented by.
Flow Over Immersed Bodies
Fluid Friction. Outline Bernoulli ’ s Equation The Pressure-Drop Experiment Laminar Flow Turbulent Flow The Three Friction Factor Problems Computer Methods.
Dr. Laila Guessous Suresh Putta, M.S. Student Numerical Investigations of Pulsatile Flows To develop a better understanding of the characteristics of pulsating.
WP4: Safety and Performance for Innovative Reactor Systems 3 rd Annual Meeting, Imperial College London, 9 th April 2008 Reynolds-Averaged Navier-Stokes.
1 Progress on the v2f model with Code_Saturne EDF - Manchester meeting 18-19th May 2009.
Work progress Dalila AMMOUR Buoyant flow inside penetration cavity Numerical procedure: Code used: Code_Saturne V1.4.0 Model used actually: K-eps standard.
Introduction to Convection: Flow and Thermal Considerations
EdF meeting 18 May 2009 Review of all the work done under the framework of Code_Saturne by S. Rolfo School of Mechanical, Aerospace & Civil Engineering.
Hydraulic Analysis of STHE Using Bell Delaware Method
© Fluent Inc. 8/10/2015G1 Fluids Review TRN Heat Transfer.
Introduction to Convection: Flow and Thermal Considerations
Introduction to COMSOL Travis Campbell Developed for CHE 331 – Fall 2012 Oregon State University School of Chemical, Biological and Environmental Engineering.
Matthew Fischels Aerospace Engineering Department Major Professor : Dr. R. Ganesh Rajagopalan REDUCING RUNTIME OF WIND TURBINE SIMULATION Los Alamos National.
Miguel Talavera Fangjun Shu
Wind Energy Program School of Aerospace Engineering Georgia Institute of Technology Computational Studies of Horizontal Axis Wind Turbines PRINCIPAL INVESTIGATOR:
Introduction to Fluid Mechanics
Endwall Contouring, Using Continuous Diffusion Technology, A Breakthrough Technology and its Application to a Three-Stage High Pressure Turbine Introduced.
Solving Energy problems.  A 0.1-kg baseball has 20 joules of kinetic energy as it passes over the plate. How fast is it moving?
Cascade Flow Research Capability Following figures present experimental results dealing with the measurement of boundary layer development along the suction.
Chapter 6 Introduction to Forced Convection:
2004Fluid Mechanics II Prof. António Sarmento - DEM/IST u Contents: –1/7 velocity law; –Equations for the turbulent boundary layer with zero pressure gradient.
Fluid Report Presentation Onur Erkal Korgun Koyunpınar Korhan Türker Hakan Uzuner.
Introduction to Fluid Mechanics
IB Physics Topic 8 – Solar and Wind 3 Mr. Jean. The plan: Video clip of the day Energy production –Solar Power –Wind Power.
CFX-10 Introduction Lecture 1.
© Pritchard Introduction to Fluid Mechanics Chapter 8 Internal Incompressible Viscous Flow.
Compressor Cascade Pressure Rise Prediction
SPARTAN Chamber Dynamics Code Zoran Dragojlovic and Farrokh Najmabadi University of California in San Diego HAPL Meeting, June 20-21, 2005, Lawrence Livermore.
Reynolds Analogy It can be shown that, under specific conditions (no external pressure gradient and Prandtle number equals to one), the momentum and heat.
Compressible Frictional Flow Past Wings P M V Subbarao Professor Mechanical Engineering Department I I T Delhi A Small and Significant Region of Curse.
INTRODUCTION TO CONVECTION
Turbulence Models Validation in a Ventilated Room by a Wall Jet Guangyu Cao Laboratory of Heating, Ventilating and Air-Conditioning,
Wind Energy Program School of Aerospace Engineering Georgia Institute of Technology Computational Studies of Horizontal Axis Wind Turbines PRINCIPAL INVESTIGATOR:
SPH weekly meeting Free surface flows in Code Saturne Results 23/11/2009 Olivier Cozzi.
IB Physics Topic 8 Mr. Jean March 3 rd, The plan: Video clip of the day Energy production –Solar Power –Wind Power –Water Power.
EOLEO = Aerodynamic s + Solar Energy + Wind’s Energy.
Heat Transfer Su Yongkang School of Mechanical Engineering # 1 HEAT TRANSFER CHAPTER 7 External flow.
CONVECTION : An Activity at Solid Boundary P M V Subbarao Associate Professor Mechanical Engineering Department IIT Delhi Identify and Compute Gradients.
Introduction to Fluid Mechanics
External flow: drag and Lift
CGS Ground School Principles Of Flight Drag © Crown Copyright 2012
The k-ε model The k-ε model focuses on the mechanisms that affect the turbulent kinetic energy (per unit mass) k. The instantaneous kinetic energy k(t)
Fluid Mechanics & Hydraulics
Penetration Buoyant flow inside cavity Conference paper UKHTC 2011
IB Physics Topic 8 Mr. Jean March 5th, 2014.
Viscous Flow in Pipes.
CHAPTER 6 Viscous Flow in Pipes
Deposition and Removal
Transition of the laminar boundary layer on a flat plate into a fully turbulent boundary layer (not to scale). Trip Wires:
Lecture Objectives Review for exam Discuss midterm project
Laminar and Turbulent Flow
FLUID MECHANICS REVIEW
Stationary Point Notes
Convective Heat Transfer
Section 8, Lecture 1, Supplemental Effect of Pressure Gradients on Boundary layer • Not in Anderson.
Introduction to Fluid Mechanics
Presentation transcript:

Combining the strengths of UMIST and The Victoria University of Manchester Laminar Kinetic Energy Models in Code_Saturne Presented by Clare Turner

Combining the strengths of UMIST and The Victoria University of Manchester Presentation Outline Progress of the 2 nd model Progress of the 1 st model The first test case Models for implementation Introduction to the problem Summary of actions

Combining the strengths of UMIST and The Victoria University of Manchester Industrial Application  Pressure drop in fuel assemblies  Efficiency of combustion process  Turbomachinery  Wind turbine blades Examples: Can be applied to any transition case Original application: rear wing of a Formula 1 car

Combining the strengths of UMIST and The Victoria University of Manchester Model Equations – 2005 model Walters-Leylek 2005

Combining the strengths of UMIST and The Victoria University of Manchester Model Equations – 2008 model Walters-Cokljat 2008

Combining the strengths of UMIST and The Victoria University of Manchester T3 Flat Plate Tests

Combining the strengths of UMIST and The Victoria University of Manchester Boundary conditions Inlet conditions: k = m 2 /s 2 ; ε = 1.35 m 2 /s 3 ; U = 5.08 m/s Inlet conditions determined by FSTI curve in STAR-CD

Combining the strengths of UMIST and The Victoria University of Manchester The 2005 Model: Initial Results Turbulent profile too low

Combining the strengths of UMIST and The Victoria University of Manchester Corrections in the Code (1) Incorrect wall boundary conditions

Combining the strengths of UMIST and The Victoria University of Manchester Corrections in the Code (2) Error in the paper for the laminar kinetic energy transport equation The lack of diffusion caused convergence problems

Combining the strengths of UMIST and The Victoria University of Manchester Correction of the 2005 Model (1)

Combining the strengths of UMIST and The Victoria University of Manchester Corrected Version of the 2005 Model

Combining the strengths of UMIST and The Victoria University of Manchester Further Work Required This test case has zero pressure gradient so f ΔP term has been ignored

Combining the strengths of UMIST and The Victoria University of Manchester Further Work Required The next test case has a pressure gradient, therefore the change in Ω must be calculated Currently have Ω stored as a common – similar to how S2KW is stored from visklw.F routine Is there a simple way of determining whether the gradient is positive at each cell? Also concerns about adapting to parallel computations

Combining the strengths of UMIST and The Victoria University of Manchester Differences Between Models 2005 Model2008 Model

Combining the strengths of UMIST and The Victoria University of Manchester The 2008 model: Test

Combining the strengths of UMIST and The Victoria University of Manchester Areas For Error From experience, the low profile reflects incorrect ω at the wall Looking at routines which affect this Intending to look at budgets, ω values are smaller than 2005 model

Combining the strengths of UMIST and The Victoria University of Manchester Summary Including two k L -k T -ω models (ITURB=61) For the 2004 version require inclusion of f ΔP term – require help! Errors in 2008 model, need to contact authors but also may be problems in routines – have a list of edited routines

Combining the strengths of UMIST and The Victoria University of Manchester Any Questions?