Pressure limit of hydrogen spontaneous ignition in a T-shaped channel

Size: px
Start display at page:

Download "Pressure limit of hydrogen spontaneous ignition in a T-shaped channel"

Transcription

1 4 th International Conference on Hydrogen Safety, September 2011, San Francisco, USA Pressre limit of hydrogen spontaneos ignition in a T-shaped channel Maim Bragin, Dmitriy Makarov, Vladimir Molkov Hydrogen Safety Engineering and Research (HySAFER) Centre, University of Ulster

2 Backgrond Aim and obectives Eperiment in T-shape channel (Golb et al., 2010) LES EDC model Modelling of membrane opening Instant verss finite membrane opening Simlation reslts Otline Dynamics of spontaneos ignition at different storage pressre Conclsions

3 Backgrond Pressre relief device (PRD) activation Sdden release of hydrogen into air What is the lower pressre limit for spontaneos ignition in T-shape channel (PRD mock-p)?

4 Aim and obectives Aim: Develop contemporary model for predictive simlation of the phenomenon of hydrogen spontaneos ignition dring sdden release from pressre relief devices (to be applied as a tool for hydrogen safety engineering) Obectives: Develop Large Eddy Simlation (LES) model based on the Eddy Dissipation Concept (EDC), fll chemistry, and modelling of a brst disk opening in a finite time Validate the LES EDC model and simlations against eperimental data by Golb et al. (2010) on spontaneos ignition in T-shape channel (mock-p PRD) Understand dynamics of the ignition process and eplain scattering in reported eperimental data (Golb et al., 2010) Establish the lower pressre limit for spontaneos ignition in T-shape channel

5 Eperiment (Golb et al., 2010) Brst disk rptre at storage pressres from 13.5 to 29 bar. Reported: no ignition at 13.5 bar, and spontaneos ignition at 29 bar (private commnication ignition at 24.3 bar) Brst disk ID 4 ID 16 ID 10 ID High-pressre section (hydrogen) PRD (air)

6 Comptational domain High pressre tbes PRD Eternal domain Brst disk

7 LES eqations ( ) 0 = t ρ ρ ( ) i i k k i i i i i g p t ρ δ μ ρ ρ = 3 2 ( ) ( ) ( )= p E E t ρ ρ m m m p Y Sc h T c Pr [ μ μ ( ) ( ) m m m H R Y Sc Y Y t = μ ρ ρ Continity eqation: Momentm conservation eqation: Energy conservation eqation: Species conservation eqation: m C m i k k i i i H R ] 3 2 δ μ

8 RNG trblence model The ective viscosity in RNG SGS model is calclated as μ 2 μs μ = μ 1 H μ , where μ = ( 0.157VCV ) 2Si Si In highly trblent flows, μ μ s and the RNG model redces to Smagorinsky model in laminar flow regions the argment of Heaviside fnction becomes negative and the model recovers moleclar viscosity, = μ. The ective Prandtl and Schmidt nmbers are calclated following the RNG theory by Yakhot prely from the theoretical eqation 1 1 N N μ N N S = s i = ρ μ μ 1 2 i i

9 EDC combstion model 1/2 Eddy Dissipation Concept (EDC) gives an epression for a combstion rate based on an assmption that chemical reactions occr in so-called fine strctres of Kolmogorov s scale, where the dissipation of trblence energy takes place. In EDC model a sorce term in species ( ) 2 transport eqation is modelled as: ρ ξ [ ] ( R ) m = Ym Y 3 m τ 1 ξ R m is a net rate of prodction of specie m by chemical reactions, * ξ ( ) is the length fraction of the fine scale trblent strctres where the reaction occrs, Y m is the fine scale species mass fraction (specie m) after reacting over the time, τ Y m is a species mass fraction for specie m in the srronding fine scales state.

10 The length fraction of fine strctres: ξ = η / SGS 1 3 where = μ ρ L ) and L SGS = 0.157V SGS t EDC combstion model 2/2 /( SGS 3 μ SGS and the Kolmogorov s velocity η = ρ LSGS Characteristic sb-grid eddy and Kolmogorov timescales are: 1 2 τ SGS = L SGS / SGS and τ μ L SGS = η 3 ρ SGS * The volme fraction of the fine scales is calclated as ξ 3 and species are assmed to react in the fine strctres over a time scale τ = τ η. It is assmes that all the fine scales in the cell are perfectly * stirred reactors with a residence time τ 1 4

11 Chemistry mechanism Mechanism for H2 combstion (with NO), 13 species and 37 reactions Units are cm3, mol, s, KJ and K HO2=OHO 2.E H2O=OHH 1.8E H2OO=OHOH 5.9E H2OH=H2OH 1.17E HO2M=HO2M 2.3E H2/1./ H2O/6.5/ O2/0.4/ N2/0.4/ HHO2=OHOH 1.5E HHO2=H2O2 2.5E OHHO2=H2OO2 2.E HHM=H2M 1.8E H2/1./ H2O/6.5/ O2/0.4/ N2/0.4/ HOHM=H2OM 2.2E H2/1./ H2O/6.5/ O2/0.4/ N2/0.4/ HO2HO2=H2O2O2 2.E H2O2M=OHOHM 1.3E H2O2OH=H2OHO2 1.E OHO2=OHO2 2.E HHO2=OH2O 5.E HOM=OHM 6.2E OOM=O2M 6.17E H2O2H=H2OOH 1.E H2O2H=HO2H2 4.79E OOHM=HO2M 1.E H2O2=OHOH 1.7E ON2=NNO 1.82E ONO=NO2 3.8E HNO=NOH 2.63E NOM=NOM 3.98E N2M=NNM 3.72E N2OO=NONO 6.92E N2OO=N2O2 1.E N2ON=N2NO 1.E NHO2=NOOH 1.E N2OH=N2OH 7.6E HNOO=NOOH 5.01E HNOOH=NOH2O 1.26E NOHO2=HNOO2 2.E HNOHO2=NOH2O2 3.16E HNOH=NOH2 1.26E HNOM=HNOM 1.78E GUTHEIL, E., BALAKRISHNAN, G. & WILLIAMS, F. A. (1993) Strctre and etinction of hydrogen-air diffsion flames. IN PETERS, N. & ROGG, B. (Eds.) Redced kinetic mechanisms for applications in combstion systems. New York, Springer-Verlag

12 Brst disk opening sections Brst disk opening process was approimated by a 10 step process. Sections were open from 1 to 10 at times calclated according to the table in the net slide.

13 Brst disk opening time Following Spence & Woods (1964), the following formla was sed to obtain the rptre time of a brst disk: t = ρbd k p 1 2 where ρ the density of the diaphragm material (annealed copper), b and d are the thickness and the diameter of the diaphragm, k constant, 0.92 p driving pressre Opening times of sections for each of the simlations are listed below: Section Opening time, μs [1.35 MPa case] Opening time, μs [1.65 MPa case] Opening time, μs [2.43 MPa case] Opening time, μs [2.9 MPa case]

14 Instant vs finite opening time

15 Simlation reslts

16 P=29 bar Ignition initiated in the radial vent channel and etingished. Combstion is reinitiated in a nmber of spots otside the PRD. Concentration of hydrogen in these spots st before the ignition is in the range 29-36% by vol.

17 P=24.3 bar Ignition is initiated in the radial channel (closer to the pstream wall second shock reflection) similar to 29 bar case Reignition otside is not observed. Process took 10μs and was eperimentally registered ( ignition in private commnication)

18 P=16.5 bar Temperatre Ignition spot is located in the aial channel (not in a symmetry plane). The combstion propagates pstream (ntil oygen is consmed)! Iso-srfaces are: Ble 550 K, Green 1500 K, Red 2400 K

19 P=16.5 bar OH mole fraction Ignition is confirmed by a hydroyl mole fraction distribtion. Light sensor in eperiments was located otside and cold not have registered ignition. Iso-srfaces are: Ble , Green 0.002, Red 0.02

20 P=13.5 bar no ignition Hydroyl mole fraction is (not shown). Note: temperatre scale is different in this pictre.

21 Conclsions The LES model based on EDC with detailed kinetics and inertial brst disk was sccessflly applied to reprodce and eplain eperimental observations in T-shape channel (PRD mock-p). The lower pressre limit for spontaneos ignition in a T- shaped PRD is established: there is no ignition at storage pressre 13.5 bar; there is ignition followed by selfetinction at pressres 16.5 and 24.3 bar; and there is sstainable ignition (reignition otside the channel) for storage pressre 29 bar. The ignition is located in the are of the second reflection of initial shock and where the concentration of hydrogen in air is in the range 29-36% vol. The model can be sed as a contemporary tool for design of innovative pressre relief devices.

22 MSc in Hydrogen Safety Engineering (distance learning corse): 22

Lewis number and curvature effects on sound generation by premixed flame annihilation

Lewis number and curvature effects on sound generation by premixed flame annihilation Center for Trblence Research Proceedings of the Smmer Program 2 28 Lewis nmber and crvatre effects on sond generation by premixed flame annihilation By M. Talei, M. J. Brear AND E. R. Hawkes A nmerical

More information

On the importance of horizontal turbulent transport in high resolution mesoscale simulations over cities. A. Martilli (CIEMAT, Spain), B. R.

On the importance of horizontal turbulent transport in high resolution mesoscale simulations over cities. A. Martilli (CIEMAT, Spain), B. R. On the importance of horizontal trblent transport in high resoltion mesoscale simlations over cities. A. Martilli (CIEMAT, Spain), B. R. Rotnno, P. Sllivan, E. G. Patton, M. LeMone (NCAR, USA) In an rban

More information

Wall treatment in Large Eddy Simulation

Wall treatment in Large Eddy Simulation Wall treatment in arge Edd Simlation David Monfort Sofiane Benhamadoche (ED R&D) Pierre Sagat (Université Pierre et Marie Crie) 9 novembre 007 Code_Satrne User Meeting Wall treatment in arge Edd Simlation

More information

Course Outline. Boundary Layer Flashback Core Flow Flashback and Combustion Induced Vortex Breakdown

Course Outline. Boundary Layer Flashback Core Flow Flashback and Combustion Induced Vortex Breakdown Corse Otline A) Introdction and Otlook B) Flame Aerodynamics and Flashback C) Flame Stretch, Edge Flames, and Flame Stabilization Concepts D) Distrbance Propagation and Generation in Reacting Flows E)

More information

Spring Semester 2011 April 5, 2011

Spring Semester 2011 April 5, 2011 METR 130: Lectre 4 - Reynolds Averaged Conservation Eqations - Trblent Flxes (Definition and typical ABL profiles, CBL and SBL) - Trblence Closre Problem & Parameterization Spring Semester 011 April 5,

More information

Modeling Effort on Chamber Clearing for IFE Liquid Chambers at UCLA

Modeling Effort on Chamber Clearing for IFE Liquid Chambers at UCLA Modeling Effort on Chamber Clearing for IFE Liqid Chambers at UCLA Presented by: P. Calderoni own Meeting on IFE Liqid Wall Chamber Dynamics Livermore CA May 5-6 3 Otline his presentation will address

More information

5.1 Heat removal by coolant flow

5.1 Heat removal by coolant flow 5. Convective Heat Transfer 5.1 Heat removal by coolant flow Fel pellet Bond layer Cladding tbe Heat is transferred from the srfaces of the fel rods to the coolant. T Temperatre at center of fc fel pellet

More information

NATURAL CONVECTION No mechanical force to push the fluid pump, fan etc. No predefined fluid flowrate and velocity can t prescribe Reynolds

NATURAL CONVECTION No mechanical force to push the fluid pump, fan etc. No predefined fluid flowrate and velocity can t prescribe Reynolds NATURA CONVECTION No mechanical force to psh the flid pmp, fan etc. No predefined flid flowrate and velocit can t prescribe Renolds nmber Flid moves as a reslt of densit difference Flid velocit established

More information

PROBLEMS

PROBLEMS PROBLEMS------------------------------------------------ - 7- Thermodynamic Variables and the Eqation of State 1. Compter (a) the nmber of moles and (b) the nmber of molecles in 1.00 cm of an ideal gas

More information

Burning Rate, Kinetic Coupling, and Mechanism Reduction

Burning Rate, Kinetic Coupling, and Mechanism Reduction Brning Rate, Kinetic Copling, and Mechanism Redction Yigang J Mechanical and Aerospace Engineering Princeton University 27 AFOSR MURI Kick-Off Meeting Generation of Comprehensive Srrogate Kinetic Models

More information

CFD-Simulation thermoakustischer Resonanzeffekte zur Bestimmung der Flammentransferfunktion

CFD-Simulation thermoakustischer Resonanzeffekte zur Bestimmung der Flammentransferfunktion CFD-Simlation thermoakstischer Resonanzeffekte zr Bestimmng der Flammentransferfnktion Ator: Dennis Paschke Technische Universität Berlin Institt für Strömngsmechanik nd Technische Akstik FG Experimentelle

More information

Reducing the Carbon Footprint of Transportation Fuels through Computational Modelling

Reducing the Carbon Footprint of Transportation Fuels through Computational Modelling Reducing the Carbon Footprint of Transportation Fuels through Computational Modelling http://www.conserve-energy-future.com Computational Modelling Group Founded in 1999 Head Prof. Currently 20 members

More information

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA. PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 13 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA. PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 13 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS EDEXCEL NATIONAL CERTIFICATE/DIPLOMA PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 3 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS TUTORIAL - PIPE FLOW CONTENT Be able to determine the parameters of pipeline

More information

Turbulence and boundary layers

Turbulence and boundary layers Trblence and bondary layers Weather and trblence Big whorls hae little whorls which feed on the elocity; and little whorls hae lesser whorls and so on to iscosity Lewis Fry Richardson Momentm eqations

More information

Applying Laminar and Turbulent Flow and measuring Velocity Profile Using MATLAB

Applying Laminar and Turbulent Flow and measuring Velocity Profile Using MATLAB IOS Jornal of Mathematics (IOS-JM) e-issn: 78-578, p-issn: 319-765X. Volme 13, Isse 6 Ver. II (Nov. - Dec. 17), PP 5-59 www.iosrjornals.org Applying Laminar and Trblent Flow and measring Velocity Profile

More information

THE ACOUSTIC RESPONSE OF BURNER-STABILIZED PREMIXED FLAT FLAMES

THE ACOUSTIC RESPONSE OF BURNER-STABILIZED PREMIXED FLAT FLAMES Proceedings of the Combstion Institte, Volme 29, 2002/pp. 115 122 THE ACOUSTIC RESPONSE OF BURNER-STABILIZED PREMIXED FLAT FLAMES K. R. A. M. SCHREEL, R. ROOK and L. P. H. DE GOEY Eindhoven University

More information

Microscale physics of fluid flows

Microscale physics of fluid flows Microscale physics of flid flows By Nishanth Dongari Senior Undergradate Department of Mechanical Engineering Indian Institte of Technology, Bombay Spervised by Dr. Sman Chakraborty Ot line What is microflidics

More information

Microscopic Properties of Gases

Microscopic Properties of Gases icroscopic Properties of Gases So far we he seen the gas laws. These came from observations. In this section we want to look at a theory that explains the gas laws: The kinetic theory of gases or The kinetic

More information

Numerical Simulation of Three Dimensional Flow in Water Tank of Marine Fish Larvae

Numerical Simulation of Three Dimensional Flow in Water Tank of Marine Fish Larvae Copyright c 27 ICCES ICCES, vol.4, no.1, pp.19-24, 27 Nmerical Simlation of Three Dimensional Flo in Water Tank of Marine Fish Larvae Shigeaki Shiotani 1, Atsshi Hagiara 2 and Yoshitaka Sakakra 3 Smmary

More information

Two identical, flat, square plates are immersed in the flow with velocity U. Compare the drag forces experienced by the SHADED areas.

Two identical, flat, square plates are immersed in the flow with velocity U. Compare the drag forces experienced by the SHADED areas. Two identical flat sqare plates are immersed in the flow with velocity U. Compare the drag forces experienced by the SHAE areas. F > F A. A B F > F B. B A C. FA = FB. It depends on whether the bondary

More information

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION Rssell Qadros, Krishnend Sinha Department of Aerospace Engineering Indian Institte of Technology Bombay Mmbai, India 476 Johan

More information

4 Exact laminar boundary layer solutions

4 Exact laminar boundary layer solutions 4 Eact laminar bondary layer soltions 4.1 Bondary layer on a flat plate (Blasis 1908 In Sec. 3, we derived the bondary layer eqations for 2D incompressible flow of constant viscosity past a weakly crved

More information

Toward a multilevel QM/MM methodology for performing molecular dynamic simulations of complex reactive processes

Toward a multilevel QM/MM methodology for performing molecular dynamic simulations of complex reactive processes Toward a multilevel QM/MM methodology for performing molecular dynamic simulations of complex reactive processes Michael R. Salazar Department of Chemistry Union University, Jackson, TN 38305 msalazar@uu.edu

More information

Uncertainties of measurement

Uncertainties of measurement Uncertainties of measrement Laboratory tas A temperatre sensor is connected as a voltage divider according to the schematic diagram on Fig.. The temperatre sensor is a thermistor type B5764K [] with nominal

More information

ρ u = u. (1) w z will become certain time, and at a certain point in space, the value of

ρ u = u. (1) w z will become certain time, and at a certain point in space, the value of THE CONDITIONS NECESSARY FOR DISCONTINUOUS MOTION IN GASES G I Taylor Proceedings of the Royal Society A vol LXXXIV (90) pp 37-377 The possibility of the propagation of a srface of discontinity in a gas

More information

Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction

Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction A. Ahmed, M. N.Sarki, M. Ahmad Abstract In this paper the stdy of nsteady flow

More information

MEASUREMENT OF TURBULENCE STATISTICS USING HOT WIRE ANEMOMETRY

MEASUREMENT OF TURBULENCE STATISTICS USING HOT WIRE ANEMOMETRY MEASUREMENT OF TURBULENCE STATISTICS USING HOT WIRE ANEMOMETRY Mrgan Thangadrai +, Atl Kmar Son *, Mritynjay Singh +, Sbhendra *, Vinoth Kmar ++, Ram Pyare Singh +, Pradip K Chatterjee + + Thermal Engineering,

More information

Numerical Model for Studying Cloud Formation Processes in the Tropics

Numerical Model for Studying Cloud Formation Processes in the Tropics Astralian Jornal of Basic and Applied Sciences, 5(2): 189-193, 211 ISSN 1991-8178 Nmerical Model for Stdying Clod Formation Processes in the Tropics Chantawan Noisri, Dsadee Skawat Department of Mathematics

More information

CHAPTER 8 CONVECTION IN EXTERNAL TURBULENT FLOW

CHAPTER 8 CONVECTION IN EXTERNAL TURBULENT FLOW CHAPTER 8 CONVECTION IN EXTERNAL TURBULENT FLOW 8.1 Introdction Common phsical phenomenon, bt comple Still relies on empirical data and rdimentar conceptal drawings Tremendos growth in research over last

More information

Chapter 1: Differential Form of Basic Equations

Chapter 1: Differential Form of Basic Equations MEG 74 Energ and Variational Methods in Mechanics I Brendan J. O Toole, Ph.D. Associate Professor of Mechanical Engineering Howard R. Hghes College of Engineering Universit of Nevada Las Vegas TBE B- (7)

More information

DILUTE GAS-LIQUID FLOWS WITH LIQUID FILMS ON WALLS

DILUTE GAS-LIQUID FLOWS WITH LIQUID FILMS ON WALLS Forth International Conference on CFD in the Oil and Gas, Metallrgical & Process Indstries SINTEF / NTNU Trondheim, Noray 6-8 Jne 005 DILUTE GAS-LIQUID FLOWS WITH LIQUID FILMS ON WALLS John MORUD 1 1 SINTEF

More information

5. The Bernoulli Equation

5. The Bernoulli Equation 5. The Bernolli Eqation [This material relates predominantly to modles ELP034, ELP035] 5. Work and Energy 5. Bernolli s Eqation 5.3 An example of the se of Bernolli s eqation 5.4 Pressre head, velocity

More information

Theoretical study on impingement heat transfer with single-phase free-surface slot jets

Theoretical study on impingement heat transfer with single-phase free-surface slot jets International Jornal of Heat and Mass Transfer 4 (25) 331 336 www.elsevier.com/locate/ijhmt Theoretical stdy on impingement heat transfer with single-phase free-srface slot jets Y.C. Chen, C.F. Ma *, M.

More information

UNIT V BOUNDARY LAYER INTRODUCTION

UNIT V BOUNDARY LAYER INTRODUCTION UNIT V BOUNDARY LAYER INTRODUCTION The variation of velocity from zero to free-stream velocity in the direction normal to the bondary takes place in a narrow region in the vicinity of solid bondary. This

More information

SIMULATION OF TURBULENT FLOW AND HEAT TRANSFER OVER A BACKWARD-FACING STEP WITH RIBS TURBULATORS

SIMULATION OF TURBULENT FLOW AND HEAT TRANSFER OVER A BACKWARD-FACING STEP WITH RIBS TURBULATORS THERMAL SCIENCE, Year 011, Vol. 15, No. 1, pp. 45-55 45 SIMULATION OF TURBULENT FLOW AND HEAT TRANSFER OVER A BACKWARD-FACING STEP WITH RIBS TURBULATORS b Khdheer S. MUSHATET Mechanical Engineering Department,

More information

BLOOM S TAXONOMY. Following Bloom s Taxonomy to Assess Students

BLOOM S TAXONOMY. Following Bloom s Taxonomy to Assess Students BLOOM S TAXONOMY Topic Following Bloom s Taonomy to Assess Stdents Smmary A handot for stdents to eplain Bloom s taonomy that is sed for item writing and test constrction to test stdents to see if they

More information

Hybrid modelling and model reduction for control & optimisation

Hybrid modelling and model reduction for control & optimisation Hybrid modelling and model redction for control & optimisation based on research done by RWTH-Aachen and TU Delft presented by Johan Grievink Models for control and optimiation market and environmental

More information

An Experimental Facility for Studying Flame Propagation at Elevated Pressures

An Experimental Facility for Studying Flame Propagation at Elevated Pressures Paper # 7LT-21 Topic: Laminar and Trblent Flames 8 th U. S. National Combstion Meeting Organized by the Western States Section of the Combstion Institte and hosted by the University of Utah May 19-22,

More information

Material Transport with Air Jet

Material Transport with Air Jet Material Transport with Air Jet Dr. István Patkó Bdapest Tech Doberdó út 6, H-1034 Bdapest, Hngary patko@bmf.h Abstract: In the field of indstry, there are only a very few examples of material transport

More information

Quantitative Characterization of Pressure-related Turbulence Transport Terms using Simultaneous Nonintrusive Pressure and Velocity Measurement*

Quantitative Characterization of Pressure-related Turbulence Transport Terms using Simultaneous Nonintrusive Pressure and Velocity Measurement* Qantitative Characterization of Pressre-related Trblence Transport Terms sing Simltaneos Nonintrsive Pressre and Velocity Measrement* Xiaofeng Li and Joseph Katz Department of Aerospace Engineering San

More information

A Model-Free Adaptive Control of Pulsed GTAW

A Model-Free Adaptive Control of Pulsed GTAW A Model-Free Adaptive Control of Plsed GTAW F.L. Lv 1, S.B. Chen 1, and S.W. Dai 1 Institte of Welding Technology, Shanghai Jiao Tong University, Shanghai 00030, P.R. China Department of Atomatic Control,

More information

Computational Fluid Dynamics Simulation and Wind Tunnel Testing on Microlight Model

Computational Fluid Dynamics Simulation and Wind Tunnel Testing on Microlight Model Comptational Flid Dynamics Simlation and Wind Tnnel Testing on Microlight Model Iskandar Shah Bin Ishak Department of Aeronatics and Atomotive, Universiti Teknologi Malaysia T.M. Kit Universiti Teknologi

More information

A Decomposition Method for Volume Flux. and Average Velocity of Thin Film Flow. of a Third Grade Fluid Down an Inclined Plane

A Decomposition Method for Volume Flux. and Average Velocity of Thin Film Flow. of a Third Grade Fluid Down an Inclined Plane Adv. Theor. Appl. Mech., Vol. 1, 8, no. 1, 9 A Decomposition Method for Volme Flx and Average Velocit of Thin Film Flow of a Third Grade Flid Down an Inclined Plane A. Sadighi, D.D. Ganji,. Sabzehmeidani

More information

HOW TO USE CHEMKIN 경원테크

HOW TO USE CHEMKIN 경원테크 HOW TO USE CHEMKIN 경원테크 Agenda CHEMKIN-PRO vs. Old Chemkin II CHEMKIN-PRO Overview Advanced Feature: Particle Tracking Advanced Feature: Reaction Path Analysis Example : Turbulent jet with kinetics & mixing

More information

Lift-Off and Blow-Out of Under-Expanded Hydrogen Jets: Experiments versus Simulations

Lift-Off and Blow-Out of Under-Expanded Hydrogen Jets: Experiments versus Simulations Lift-Off and Blow-Out of Under-Expanded Hydrogen Jets: Experiments versus Simulations Shentsov V. 1, *, Sakatsume R. 2, Makarov D. 1, Takeno K. 2, Molkov V. 1 1 University of Ulster, Hydrogen Safety Engineering

More information

The Numerical Simulation of Enhanced Heat Transfer Tubes

The Numerical Simulation of Enhanced Heat Transfer Tubes Aailable online at.sciencedirect.com Phsics Procedia 4 (01 70 79 01 International Conference on Applied Phsics and Indstrial Engineering The Nmerical Simlation of Enhanced Heat Transfer Tbes Li Xiaoan,

More information

Prandl established a universal velocity profile for flow parallel to the bed given by

Prandl established a universal velocity profile for flow parallel to the bed given by EM 0--00 (Part VI) (g) The nderlayers shold be at least three thicknesses of the W 50 stone, bt never less than 0.3 m (Ahrens 98b). The thickness can be calclated sing Eqation VI-5-9 with a coefficient

More information

Parametrization of turbulent fluxes in the outer layer

Parametrization of turbulent fluxes in the outer layer Parametriation of trblent flxes in the oter layer Irina Sand Oerie of models Blk models Local -closre -profile closre 0 order 1 st order ED/F closre non-local TE closre 1.5 th order Crrent closre in the

More information

Process Modeling of Wellbore Leakage for GCS Risk Assessment

Process Modeling of Wellbore Leakage for GCS Risk Assessment Process Modeling of Wellbore Leakage for CS Risk Assessment Crtis M. Oldenbrg Earth Sciences Division Lawrence Berkeley National Laboratory Contribtors: Leha Pan (LBNL) Bill Carey (LANL) IEAH- Modeling

More information

IJAET International Journal of Application of Engineering and Technology ISSN: Vol.1 No.1

IJAET International Journal of Application of Engineering and Technology ISSN: Vol.1 No.1 IJAET International Jornal of Application of Engineering and Technology ISSN: 395-3594 Vol1 No1 ANALYSIS OF SUPERSONIC FLOWS IN THE E -LAVAL NOZZLE AT 1 INTO A SUENLY EXPANE UCT AT L/=WITH CAVITY ASPECT

More information

Large Eddy Simulation Of Flow Past A Two-dimensional Hill

Large Eddy Simulation Of Flow Past A Two-dimensional Hill Large Eddy Simlation Of Flow Past A Two-dimensional Hill Sankara N.Vengadesan ) and Akihiko Nakayama ) ) Research Associate, Email: vengades@kobe-.ac.jp, ) Professor, Email: nakayama@kobe-.ac.jp Gradate

More information

FEA Solution Procedure

FEA Solution Procedure EA Soltion Procedre (demonstrated with a -D bar element problem) EA Procedre for Static Analysis. Prepare the E model a. discretize (mesh) the strctre b. prescribe loads c. prescribe spports. Perform calclations

More information

Toward a multilevel QM/MM methodology for performing molecular dynamic simulations of complex reactive processes

Toward a multilevel QM/MM methodology for performing molecular dynamic simulations of complex reactive processes Toward a multilevel QM/MM methodology for performing molecular dynamic simulations of complex reactive processes Michael R. Salazar Department of Chemistry Union University, Jackson, TN 38305 msalazar@uu.edu

More information

International Journal of Scientific & Engineering Research, Volume 5, Issue 3, March ISSN

International Journal of Scientific & Engineering Research, Volume 5, Issue 3, March ISSN International Jornal of Scientific & Engineering Research, Volme 5, Isse 3, March-4 83 ISSN 9-558 Doble Dispersion effects on free convection along a vertical Wavy Srface in Poros Media with Variable Properties

More information

DELFT UNIVERSITY OF TECHNOLOGY

DELFT UNIVERSITY OF TECHNOLOGY DELFT UNIVERSITY OF TECHNOLOGY REPORT 02-01 The Krylov accelerated SIMPLER method for incompressible flow C. Vik and A. Saghir ISSN 1389-6520 Reports of the Department of Applied Mathematical Analysis

More information

arxiv: v1 [physics.flu-dyn] 4 Sep 2013

arxiv: v1 [physics.flu-dyn] 4 Sep 2013 THE THREE-DIMENSIONAL JUMP CONDITIONS FOR THE STOKES EQUATIONS WITH DISCONTINUOUS VISCOSITY, SINGULAR FORCES, AND AN INCOMPRESSIBLE INTERFACE PRERNA GERA AND DAVID SALAC arxiv:1309.1728v1 physics.fl-dyn]

More information

Flood flow at the confluence of compound river channels

Flood flow at the confluence of compound river channels Rier Basin Management VIII 37 Flood flow at the conflence of compond rier channels T. Ishikawa 1, R. Akoh 1 & N. Arai 2 1 Department of Enironmental Science and Technology, Tokyo Institte of Technology,

More information

Study of the diffusion operator by the SPH method

Study of the diffusion operator by the SPH method IOSR Jornal of Mechanical and Civil Engineering (IOSR-JMCE) e-issn: 2278-684,p-ISSN: 2320-334X, Volme, Isse 5 Ver. I (Sep- Oct. 204), PP 96-0 Stdy of the diffsion operator by the SPH method Abdelabbar.Nait

More information

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec First International Symposim on Fltter and its Application, 1 11 IEXPERIMENTAL STUDY ON TURBULENCE PARTIAL SIMULATION FOR BLUFF BODY Hiroshi Katschi +1 and Hitoshi Yamada + +1 Yokohama National University,

More information

Residual Currents Induced by Asymmetric Tidal Mixing in Weakly Stratified Narrow Estuaries

Residual Currents Induced by Asymmetric Tidal Mixing in Weakly Stratified Narrow Estuaries SEPTEMBER 21 C H E N G E T A L. 2135 Residal Crrents Indced by Asymmetric Tidal Mixing in Weakly Stratified Narrow Estaries PENG CHENG* AND ARNOLDO VALLE-LEVINSON Department of Civil Coastal Engineering,

More information

Fundamentals of magnetohydrodynamics

Fundamentals of magnetohydrodynamics Fndamentals of magnetohydrodynamics Part II Daniel Gómez 1, Email: dgomez@df.ba.ar Webpage: astro.df.ba.ar (1 Institto de Astronomía y Física del Espacio, CONICET, Argentina ( Departamento de Física, Universidad

More information

2 nd Joint Summer School on Fuel Cell and Hydrogen Technology September 2012, Crete, Greece. Hydrogen fires

2 nd Joint Summer School on Fuel Cell and Hydrogen Technology September 2012, Crete, Greece. Hydrogen fires 2 nd Joint Summer School on Fuel Cell and Hydrogen Technology 17 28 September 2012, Crete, Greece Hydrogen fires Sile Brennan (on behalf of the HySAFER group) Hydrogen Safety Engineering and Research Centre

More information

Momentum Equation. Necessary because body is not made up of a fixed assembly of particles Its volume is the same however Imaginary

Momentum Equation. Necessary because body is not made up of a fixed assembly of particles Its volume is the same however Imaginary Momentm Eqation Interest in the momentm eqation: Qantification of proplsion rates esign strctres for power generation esign of pipeline systems to withstand forces at bends and other places where the flow

More information

CHEMICAL REACTION EFFECTS ON FLOW PAST AN EXPONENTIALLY ACCELERATED VERTICAL PLATE WITH VARIABLE TEMPERATURE. R. Muthucumaraswamy and V.

CHEMICAL REACTION EFFECTS ON FLOW PAST AN EXPONENTIALLY ACCELERATED VERTICAL PLATE WITH VARIABLE TEMPERATURE. R. Muthucumaraswamy and V. International Jornal of Atomotive and Mechanical Engineering (IJAME) ISSN: 9-8649 (int); ISSN: 18-166 (Online); Volme pp. 31-38 Jly-December 1 niversiti Malaysia Pahang DOI: http://dx.doi.org/1.158/ijame..11.11.19

More information

High speed analysis of high pressure combustion in a constant volume cell

High speed analysis of high pressure combustion in a constant volume cell High speed analysis of high pressre combstion in a constant volme cell.j.m. Frijters *, R.J.H. Klein-Dowel, S.S. Manski, L.M.T. Somers and R.S.G. Baert Section Combstion Technology Eindhoven University

More information

Sources of Non Stationarity in the Semivariogram

Sources of Non Stationarity in the Semivariogram Sorces of Non Stationarity in the Semivariogram Migel A. Cba and Oy Leangthong Traditional ncertainty characterization techniqes sch as Simple Kriging or Seqential Gassian Simlation rely on stationary

More information

Second-Order Wave Equation

Second-Order Wave Equation Second-Order Wave Eqation A. Salih Department of Aerospace Engineering Indian Institte of Space Science and Technology, Thirvananthapram 3 December 016 1 Introdction The classical wave eqation is a second-order

More information

Numerical Simulation of Heat and Mass Transfer in the Evaporation of Glycols Liquid Film along an Insulated Vertical Channel

Numerical Simulation of Heat and Mass Transfer in the Evaporation of Glycols Liquid Film along an Insulated Vertical Channel Colmbia nternational Pblishing American Jornal of Heat and Mass Transfer doi:1.7726/ajhmt.215.15 Research Article Nmerical Simlation of Heat and Mass Transfer in the Evaporation of lcols iqid Film along

More information

FLUID FLOW FOR CHEMICAL ENGINEERING

FLUID FLOW FOR CHEMICAL ENGINEERING EKC FLUID FLOW FOR CHEMICL ENGINEERING CHTER 8 (SOLUTION WI EXERCISE): TRNSORTTION SYSTEM & FLUID METERING Dr Mohd zmier hmad Tel: +60 (4) 5996459 Email: chazmier@eng.sm.my . Benzene at 7.8 o C is pmped

More information

Proceedings of the ASME nd International Conference on Ocean, Offshore and Arctic Engineering OMAE2013 June 9-14, 2013, Nantes, France

Proceedings of the ASME nd International Conference on Ocean, Offshore and Arctic Engineering OMAE2013 June 9-14, 2013, Nantes, France Proceedings of the ASME 203 32nd International Conference on Ocean, Offshore and Arctic Engineering OMAE203 Jne 9-4, 203, Nantes, France OMAE203-0207 THE EFFICIENCY OF TIDAL FENCES: A BRIEF REVIEW AND

More information

FLUID MECHANICS D203 SAE SOLUTIONS TUTORIAL 2 APPLICATIONS OF BERNOULLI SELF ASSESSMENT EXERCISE 3

FLUID MECHANICS D203 SAE SOLUTIONS TUTORIAL 2 APPLICATIONS OF BERNOULLI SELF ASSESSMENT EXERCISE 3 FLUI MEHNIS 0 SE SOLUTIONS TUTORIL PPLITIONS OF ERNOULLI SELF SSESSMENT EXERISE Take the density of water to be 997 kg/m throghot nless otherwise stated.. Ventri meter is 50 mm bore diameter at inlet and

More information

The Bow Shock and the Magnetosheath

The Bow Shock and the Magnetosheath Chapter 6 The Bow Shock and the Magnetosheath The solar wind plasma travels sally at speeds which are faster than any flid plasma wave relative to the magnetosphere. Therefore a standing shock wave forms

More information

M. Moeini 1 and M. R. Chamani 2. Department of Civil Engineering, Amirkabir University of Technology, Tehran, Iran 2

M. Moeini 1 and M. R. Chamani 2. Department of Civil Engineering, Amirkabir University of Technology, Tehran, Iran 2 Jornal of Applied Flid Mechanics, Vol. 1, No. 4, pp. 171-177, 17. Available online at www.jafmonline.net, ISSN 1735-357, EISSN 1735-3645. DOI: 1.18869/acadpb.jafm.73.41.7544 New Perspectives on the Laminar

More information

Numerical Study on Bouncing and Separation Collision Between Two Droplets Considering the Collision-Induced Breakup

Numerical Study on Bouncing and Separation Collision Between Two Droplets Considering the Collision-Induced Breakup Jornal of Mechanical Science and Technology (007) 585~59 Jornal of Mechanical Science and Technology Nmerical Stdy on Boncing and Separation Collision Between Two Droplets Considering the Collision-Indced

More information

Lift-off and blow-out of under-expanded hydrogen jets: experiments versus simulations

Lift-off and blow-out of under-expanded hydrogen jets: experiments versus simulations Lift-off and blow-out of under-expanded hydrogen jets: experiments versus simulations Shentsov, V. 1, Sakatsume, R. 2, Makarov, D. 1, Takeno, K. 2, Molkov, V. 1 1 Hydrogen Safety Engineering and Research

More information

Proceedings of the 51st Anniversary Conference of KSME PHYSICAL MODELING OF ATMOSPHERIC FLOW AND ENVIRONMENTAL APPLICATIONS B. R.

Proceedings of the 51st Anniversary Conference of KSME PHYSICAL MODELING OF ATMOSPHERIC FLOW AND ENVIRONMENTAL APPLICATIONS B. R. Proceedings of the 51st Anniversary Conference of KSME PHYSICAL MODELING OF ATMOSPHERIC FLOW AND ENVIRONMENTAL APPLICATIONS B. R. WHITE Faclty of Mechanical and Aeronatical Engineering University of California,

More information

ScienceDirect. River morphology modeling at the downstream of Progo River post eruption 2010 of Mount Merapi

ScienceDirect. River morphology modeling at the downstream of Progo River post eruption 2010 of Mount Merapi Available online at www.sciencedirect.com ScienceDirect Procedia Environmental Sciences 8 (015 ) 148 157 The 5th Sstainable Ftre for Hman Secrity (SstaiN 014) River morphology modeling at the downstream

More information

Thermal balance of a wall with PCM-enhanced thermal insulation

Thermal balance of a wall with PCM-enhanced thermal insulation Thermal balance of a wall with PCM-enhanced thermal inslation E. Kossecka Institte of Fndamental Technological esearch of the Polish Academy of Sciences, Warsaw, Poland J. Kośny Oak idge National aboratory;

More information

Steady State and Transient Thermal Analysis of Switched Reluctance Machine

Steady State and Transient Thermal Analysis of Switched Reluctance Machine Steady State and Transient Thermal Analysis of Switched Relctance Machine E. Annie Elisabeth Jebaseeli and S. Paramasivam Abstract This paper presents the two dimensional (-D) steady state and transient

More information

Technical Note. ODiSI-B Sensor Strain Gage Factor Uncertainty

Technical Note. ODiSI-B Sensor Strain Gage Factor Uncertainty Technical Note EN-FY160 Revision November 30, 016 ODiSI-B Sensor Strain Gage Factor Uncertainty Abstract Lna has pdated or strain sensor calibration tool to spport NIST-traceable measrements, to compte

More information

Active Flux Schemes for Advection Diffusion

Active Flux Schemes for Advection Diffusion AIAA Aviation - Jne, Dallas, TX nd AIAA Comptational Flid Dynamics Conference AIAA - Active Fl Schemes for Advection Diffsion Hiroaki Nishikawa National Institte of Aerospace, Hampton, VA 3, USA Downloaded

More information

Homotopy Perturbation Method for Solving Linear Boundary Value Problems

Homotopy Perturbation Method for Solving Linear Boundary Value Problems International Jornal of Crrent Engineering and Technolog E-ISSN 2277 4106, P-ISSN 2347 5161 2016 INPRESSCO, All Rights Reserved Available at http://inpressco.com/categor/ijcet Research Article Homotop

More information

By Dr. Salah Salman. Problem (1)

By Dr. Salah Salman. Problem (1) Chemical Eng. De. Problem ( Solved Problems Samles in Flid Flow 0 A late of size 60 cm x 60 cm slides over a lane inclined to the horizontal at an angle of 0. It is searated from the lane with a film of

More information

Appendix A: The Fully Developed Velocity Profile for Turbulent Duct Flows

Appendix A: The Fully Developed Velocity Profile for Turbulent Duct Flows Appendix A: The lly Developed Velocity Profile for Trblent Dct lows This appendix discsses the hydrodynamically flly developed velocity profile for pipe and channel flows. The geometry nder consideration

More information

VIBRATION MEASUREMENT UNCERTAINTY AND RELIABILITY DIAGNOSTICS RESULTS IN ROTATING SYSTEMS

VIBRATION MEASUREMENT UNCERTAINTY AND RELIABILITY DIAGNOSTICS RESULTS IN ROTATING SYSTEMS VIBRATIO MEASUREMET UCERTAITY AD RELIABILITY DIAGOSTICS RESULTS I ROTATIG SYSTEMS. Introdction M. Eidkevicite, V. Volkovas anas University of Technology, Lithania The rotating machinery technical state

More information

Exercises in Combustion Technology

Exercises in Combustion Technology Exercises in Combustion Technology Exercise 4: Turbulent Premixed Flames Turbulent Flow: Task 1: Estimation of Turbulence Quantities Borghi-Peters diagram for premixed combustion Task 2: Derivation of

More information

A GNF framework for turbulent flow models of drag reducing fluids and proposal for a k ε type closure

A GNF framework for turbulent flow models of drag reducing fluids and proposal for a k ε type closure J. Non-Newtonian Flid Mech. 114 2003 149 184 A GNF framewor for trblent flow models of drag redcing flids and proposal for a ε type closre F. T. Pinho Centro de Estdos de Fenómenos de Transporte, DEMEGI,

More information

PhysicsAndMathsTutor.com

PhysicsAndMathsTutor.com . Two smooth niform spheres S and T have eqal radii. The mass of S is 0. kg and the mass of T is 0.6 kg. The spheres are moving on a smooth horizontal plane and collide obliqely. Immediately before the

More information

The SISTEM method. LOS ascending

The SISTEM method. LOS ascending The SISTEM method Simltaneos and Integrated Strain Tensor Estimation from geodetic and satellite deformation Measrements A new global approach to obtain three-dimensional displacement maps by integrating

More information

Transient Approach to Radiative Heat Transfer Free Convection Flow with Ramped Wall Temperature

Transient Approach to Radiative Heat Transfer Free Convection Flow with Ramped Wall Temperature Jornal of Applied Flid Mechanics, Vol. 5, No., pp. 9-1, 1. Available online at www.jafmonline.net, ISSN 175-57, EISSN 175-645. Transient Approach to Radiative Heat Transfer Free Convection Flow with Ramped

More information

Reduction of over-determined systems of differential equations

Reduction of over-determined systems of differential equations Redction of oer-determined systems of differential eqations Maim Zaytse 1) 1, ) and Vyachesla Akkerman 1) Nclear Safety Institte, Rssian Academy of Sciences, Moscow, 115191 Rssia ) Department of Mechanical

More information

Chapter 3 MATHEMATICAL MODELING OF DYNAMIC SYSTEMS

Chapter 3 MATHEMATICAL MODELING OF DYNAMIC SYSTEMS Chapter 3 MATHEMATICAL MODELING OF DYNAMIC SYSTEMS 3. System Modeling Mathematical Modeling In designing control systems we mst be able to model engineered system dynamics. The model of a dynamic system

More information

Entropy ISSN

Entropy ISSN Entrop 3, 5, 56-518 56 Entrop ISSN 199-43 www.mdpi.org/entrop/ Entrop Generation Dring Flid Flow Between wo Parallel Plates With Moving Bottom Plate Latife Berrin Erba 1, Mehmet Ş. Ercan, Birsen Sülüş

More information

Analysis of Crack Propagation in Asphalt Concrete Using Cohesive Crack Model

Analysis of Crack Propagation in Asphalt Concrete Using Cohesive Crack Model 90 TRANSPORTATION RESEARCH RECORD 1317 Analysis of Crack Propagation in Asphalt Concrete Using Cohesive Crack Model YEOU-SHANG }ENQ AND }IA-DER PERNG A cohesive crack model, which is similar to the Dgdale

More information

THE REDUCTION IN FINESTRUCTURE CONTAMINATION OF INTERNAL WAVE ESTIMATES FROM A TOWED THERMISTOR CHAIN

THE REDUCTION IN FINESTRUCTURE CONTAMINATION OF INTERNAL WAVE ESTIMATES FROM A TOWED THERMISTOR CHAIN DANIEL C. DUBBEL THE REDUCTION IN FINESTRUCTURE CONTAMINATION OF INTERNAL WAVE ESTIMATES FROM A TOWED THERMISTOR CHAIN Estimates of internal wave displacements based on towed thermistor array data have

More information

V. Hadron quantum numbers

V. Hadron quantum numbers V. Hadron qantm nmbers Characteristics of a hadron: 1) Mass 2) Qantm nmbers arising from space-time symmetries : total spin J, parity P, charge conjgation C. Common notation: 1 -- + 2 J P (e.g. for proton:

More information

Uncertainty Evaluation of Toluene Determination in Room Air by Thermal Desorption Gas Chromatography

Uncertainty Evaluation of Toluene Determination in Room Air by Thermal Desorption Gas Chromatography International Conference on Civil, Transportation and Environment (ICCTE 06) ncertainty Evalation of Tolene Determination in Room Air by Thermal Desorption Gas Chromatography Xiaoyan Wen, a,yanhi Gao,

More information

Available online at ScienceDirect. Procedia Engineering 150 (2016 )

Available online at   ScienceDirect. Procedia Engineering 150 (2016 ) Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 150 (016 ) 635 640 International Conference on Indstrial Engineering, ICIE 016 Research of Dynamics of the Rotor with Three-film

More information

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer 6. Similarit Soltions Chapter 6 Momentm Transfer in an Eternal Laminar Bondar Laer Consider a laminar incompressible bondar laer with constant properties. Assme the flow is stead and two-dimensional aligned

More information