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The role of strain and mixture fraction variance in the prediction of local extinctions The role of strain and mixture fraction variance in the prediction of local extinctions

The role of strain and mixture fraction variance in the prediction of local extinctions - PowerPoint Presentation

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The role of strain and mixture fraction variance in the prediction of local extinctions - PPT Presentation

Alessandro Soli a Ivan Langella ab Zhi X Chen c a Loughborough University Aeronautical and Automotive Engineering b Technical University of Delft Faculty of Aerospace Engineering ID: 814712

chen 2020 langella flame 2020 chen flame langella soli ukctrf annual meeting 16th september combust lr75 premixed lagrangian strain

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Slide1

The role of strain and mixture fraction variance in the prediction of local extinctions in LES of partially premixed combustion

Alessandro Solia,*, Ivan Langellaa,b, Zhi X. Chenca Loughborough University – Aeronautical and Automotive Engineering b Technical University of Delft – Faculty of Aerospace Engineeringc University of Cambridge – Department of Engineering* corresponding e-mail: a.soli@lboro.ac.uk

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020

1

Slide2

Introduction | Motivation

Mechanisms behind local extinctions yet to be fully understoodNon-premixed flames: diffusion losses > local heat releasePremixed flames: flame strained by high-vorticity regionsPartially-premixed flames: less understoodSydney/Sandia jet flame with inhomogenous inlets [1,2]Local extinctions increasing as bulk velocity risesUnstrained premixed flamelets able to predict experimental data [3]Extinctions underestimated closer to blow-off [

3]Why can we predict extinctions with an unstrained flamelets formulation?

How does the mechanism change closer to blow-off?

A. Soli, I. Langella, Z. X. Chen,

UKCTRF Annual Meeting,

16th september 2020

2

1

Barlow

et al.

,

Combust. Flame 162 (10) (2015) 3516--35402 Cutcher et al., Combust. Flame 194 (2018) 439--4513 Chen et al., Combust. Flame 212 (2020) 415--432

Slide3

Introduction | Test case

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 3Sydney/Sandia jet flame with inhomogenous inlets [1,2]

Flame

[mm]

[m/s]

[m/s]

[m/s]

[%]

Lr75-80

75

80

93.8

83.4

70

Lr75-103

75

103

120.6

107.290

FlameLr75-80758093.883.470Lr75-10375103120.6107.290

 

 

 

: bulk flow velocity

: flame blow-off velocity

 

[

3

]

1

Barlow

et al.

,

Combust. Flame

162 (10) (2015) 3516--35402 Cutcher et al., Combust. Flame 194 (2018) 439--4513 Chen et al., Combust. Flame 212 (2020) 415--432

OpenFOAM12 flow-through times per flame24h on 240 ARCHER coresTotal kAUs: 3456

Slide4

Turbulence and Combustion Modelling

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 4Favre-filtered LES equations for mass, momentum and total enthalpy

, from

transport equation

Turbulence-chemistry interactions via presumed PDF (beta functions)Database of unstrained premixed flamelets (GRI 3.0)

Transport equations for combustion variables

:

 

premixed

non-premixed

[

3

]

3

Chen

et al.

,

Combust. Flame

212 (2020) 415--432

Slide5

Turbulence and Combustion Modelling

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 5Favre-filtered LES equations for mass, momentum and total enthalpy

, with

transport equationTurbulence-chemistry interactions via presumed PDF (beta functions)Database of unstrained premixed flamelets (GRI 3.0)

Transport equations for combustion variables

:

 

4

Dunstan

et al.

,

Proc. Combust. Inst.

34 (2013) 1193—1201

5

Langella

et al.

,

Combust. Theory Model.

19 (5) (2015) 628--656

6

Langella

et al., Combust. Flame 173 (2015) 161---178

[4,5,6,…]

Slide6

Lagrangian tracking

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 6Massless Lagrangian particles injected periodically from burner mouthClassified by:origin (main vs pilot)amount of fuel (reactants mixing vs co-flow mixing)mixture fraction (in vs out of flammability limits)burning status through reaction rate and threshold

[

7]

 

extinction threshold

7

Mitarai

et al.

,

Phys. Fluids

15 (12) (2013) 3856--3866

Slide7

Results |

Lagrangian tracking | Lr75-80A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 7

injection from pilot

+

ignition

injection from main jet

+

ignition

injection from main jet

+

ignition

+

quenching67%41%7%, 1.5% stoich

.

Slide8

Results | Lagrangian

tracking | Lr75-80A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 8local extinction

injection from main jet

Slide9

Results | Lagrangian

tracking | Lr75-80A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 9local extinction

injection from main jet

interaction with cold reactants

high resolved strain

Slide10

Results | Lagrangian

tracking | Lr75-80A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 10

t = 1.38 ms

local extinction

injection from main jet

“cold”

moderate/high SGS mixing

Slide11

Results | Lagrangian

tracking | Lr75-80A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 11

t = 1.38 ms

local extinction

injection from main jet

“cold”

moderate/high SGS mixing

ms

 

ms

not enough time

to start burning!

 

Slide12

Results | Eulerian analysis | Lr75-80

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 12

t =1.72 ms

t =2.21 ms

vortex

strain

high

 

Slide13

Results | Eulerian analysis | Lr75-80

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 13How is this connected to the Lagrangian argument?Vortex-induced convective fluxes of and

Incoming

and outgoing

destabilizing for the flame

Indicates incoming cold reactants

Resolved strain aligns flame front to

destabilising

flux (

A

)Maximises

incoming cold reactants

 

Slide14

Results | Lr75-103

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 14+30% vorticity no

peak 

higher SDR

Same general

behaviour

of particles

Extinction now strain controlled

No SGS mixing mechanism

Limitation of unstrained flamelets

No SGS strain

Vorticity might be over-suppressed

Slide15

Summary

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 15LES data of partially-premixed flame [3] analysed with combined Lagrangian/Eulerian approach

Combined effect of strain and SGS mixing (through

) key mechanismLinked to large eddies casting fast packets of cold reactants on flame frontLagrangian extinction of burning particles consequence – and not cause – of extinction holes

Flamelets can predict extinctions if strain is moderate and mostly at resolved level

Limitations are scope for further modelling

 

3

Chen

et al.

,

Combust. Flame

212 (2020) 415--432

Slide16

Acknowledgements

A. Soli, I. Langella, Z. X. Chen, UKCTRF Annual Meeting, 16th september 2020 16