turbulent flames at high reyolds number -...
TRANSCRIPT
NSFProjectCBET-1703543 Dr.Song-Charng KongAFOSRProjectFA9550-16-1-0028, Dr.Chiping Li 1
JimDriscoll
AaronSkiba,TimWabel,CamCarter
TurbulentFlamesatHighReyolds Number
a) DistributedCombustion=“NearLimit”b) PilotedBunsen– RegimeDiagram=notveryNearc) JP-8flames- maybehalfway?
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DistributedTurbulentCombustion ßà Autoignition
Tianfeng Lu,JackieChen,C.K.Law
“Diluted”oxidizer=12%O2,1200K
Airat700K21%O2
Productsat2200K
Fuel
HighSpeedMixing,noflames
Auto-ignition
DistributedCombustion?
H + O2 + M à HO2 + M DME + HO2 à CH3OCH2 +H2O2
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(a)Distributedcombustion- notfoundforpilotedBunsen
Distributed?
Theory Experiments
notpreheated,notdiluted,methaneonly
TurbulenceIntensityu’/SL
Integralscale Integralscale
NoDistributed
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DistributedCombustion– howtofindit?
Distributed if:
Highlypreheated- to1200K
HighlydilutedwithproductsN2,CO2 H2O
Temperaturesriseonlyfrom1200Kto1700K
Longresidencetime =recirculation,hotwalls(Medwell,Dally)
Hi-Pilot
DistributedCombustion
PreheatTemp.(K)
ß Dilution=%O2 inreactants21%
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MichiganDISTRIBU- burner
5m=15feetTupto700K
Highlypreheatedto1200KHighlydiluted–
withN2,CO2 orH2O– to12%O2Usevitiator heater- sodilution
fractioniswellknown
Premixchamber- athighvelocitytopreventflameformation
Longresidencetime,strongmixingHotwalls
O2 injectionN2 injection
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Planfornextyear
1. CompleteMichiganDISTRIBU-burner, achievedistributedcombustion
2. ApplyourPLIFreactionratediagnostics(formaldehyde-OHoverlap,CH)
3. Measureboundariesofdistributedcombustionvs.flamelets
Hi-Pilot
DistributedCombustion
PreheatTemp.(K)
ß Dilution=%O2 inreactants21%
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b)PilotedBunsen=unheated,undilutedflamestructure
ThinWrinkledflamelets(yes)
BroadenedPreheatLayers(yes)
Fractal-like
denselypacked(yes)
Broken(yeswithpoorbacksupport)
Distributed(notunlessaddpreheat,dilution,swirl)
MichiganHi-PilotBurner- methane, notheated,notdiluted
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100m/s
Meanvelocityupto100m/su’/SL upto246Lx/δL upto215ReT =upto100,000
3.“Events”at20kHz:pulseburstlaser- OH+formald +stereoPIV
1.Reactedness structure(temperature)profilesPreheatthickness formald.&RayleighReaction layerthickness CHandoverlapTurbulenceprofiles,b.c.’s
2.MeasuredRegimeBoundaryTurbulentburningvelocity(ST)
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HighReMETHANEDataBase=temperature,preheatzones,reactionzones,turbulence
Temperature(Rayleigh)
CH10kHz
Formaldehyde20kHz
OH20kHz
turbulence(PIV)20kHz
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temperature
Largeblobsofhotproductsconvected upstreambyturbulentdiffusion
similartoDNSofJ.HChen
Reactedness (Temperature)profilesfromRayleigh
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Preheatlayerthickness
from formaldehyde PLIFalso from Rayleigh
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ReactionLayers- fromOverlapandCH
CHPLIFat10kHz
Overlapmethod
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20kHzUnsteadyEvents- simul /stereo-PIV/form.-OH
Preheat (blue), Products (red) Simultaneous Eddies,Velocity
Events:howdolargeeddiescauseDamkohler diffusionofglobsofhotgasesupstreamintoreactants?Forwhateddysize?
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Reactionlayers
CHPLIFat10kHz
Hi-PilotBurner
CamCarter’sLabTonghun Lee’slaseratAFRL
Whatisthemerging rate?pocketformationrate?
extinctionrate?
Whydoesareaneverexceedaboutfivetimes theunwrinkledarea?
Events- measurethemergingrateathighRe
CHlayers
MeasuredflameletMergingrate(M)
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PredictedRegimeBoundaries
DistributedReactions
Motivation:
Whenaremodelsvalid?
Thinflamelet modelThickenedflamelet modelDistributedreactionmodel
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Flamelets notdistributed abovepredicted“distributed” boundary
1.0
10.0
100.0
1000.0
Lx,0 /δf
u0’/SL
ThinFlamelets(Gulder)
PresentHi-Pilot data=notdistributed
LaminarWrinkledflames
Dunn,BarlowAlden=notdistributed Predicted
“Distributed”Boundary
à isnotvalidfortheseexpts.
1.0
10.0
100.0
1000.0
Lx,0 /δf
u0’/SL
Solidsymbols=MeasuredBroadenedPreheat,ThinReaction layers
Opensymbols=measured
ThinFlamelets(Gulder)
PresentHi-Pilot data
Laminar
Dunn,BarlowAldendata
MeasuredRegimeDiagram- broadeningboundary
PredictedbroadeningBoundarydoesnotagreewmeasurements
MeasuredbroadeningboundaryDT =u’Lx =180D*
CONCLUSIONSforMETHANEfuel
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1. FirstHiRedatabase- flamestructurein“Extreme” turbulenceu’/SL =240,ReT =100,000- completedimagesoftemperature,OH,formaldehyde, CH,velocity“intense” range=ReT =5,000=Dunn-Barlow,Alden(Lund)
3.MeasuredRegimeDiagram– forpilotedbunsen flamesonly
2. Broadenedpreheat,thinreactionlayersareobservedDistributedorbrokennotobservedforthisexpt.
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Broadenedpreheatlayersmeasuredtooccurwhen
DT =u’Lx =180D*
TwoboundariesonthepredictedBorghi donotmatchtheMeasuredRegimeDiagram
Brokenreactionlayersnotobserved inpresentwork- forKarlovitz numberuptofivetimesthepredictedvalue
Dunn,Masri seesomebrokenatKa =tentimespredicted
à Flamelets occurovermuchwiderrangethanpredicted
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Disclaimer- westudyTWOoutofSEVENpossiblegeometries
2.GasTurbineLPPCombustorlowmeanvelocitylargeresidence time
“DISTRIBU-burner”distributed,flameletsandextinction ?
1.Afterburnerlargemeanvelocitysmallresidencetimenotsheardominated
“High-Pilot’PilotedBunsenburnerfavorsflamelets andhardtoextinguish
Othergeometries:
3.Premixedjetflame:issheardominated
4. Bluffbody
5.Counter-flowflames
6.Sphericalflame
7.Wellstirredreactors
JP-8Flames- inprogress
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100m/s vaporized JP-8
heating tape
fine sprayDelevan atomizerliquid JP-8
5m=15feetTupto700K
JP-8premixedReT =20,000
ChemistryinHighReJP-8Flames
Pyrolysiszone
Preheatzone?
PrimaryReactionZone
WhystudyJP-8chemistryinturbulentflames?
à Onlyturbulentflames(athighRe)providerealistic
residence times =timeforfluidelementtocrossthreelayers
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Step1:PLIFofpreheatedJP-8flamesatMichigan
Fluorescenceintensity
266 nmlaserline460nm540nmwavelength
GritschONERA
Fluorescenceintensity
266 nmlaserline460nm540nm
tolueneC7H8
Sick(Michigan)
naphthalenetri-methylC10H8 benzene
PLIFofformaldehyde,OHPLIFofJP-8components:naphthalene,toluene,tri-methylbenzene
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STEP2:LineCARS- ofJimGord atAFRL
preheat
pyrolysis
primary reactions
Pumpsheet
Probesheet
Profilesof14speciesinavaporizedJP-8flame-
canitbedone?
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ChemistryinHighReJP-8Flames– jointMichigan–AFRL
pyrolysis zone imaged with JP-8 PLIF
preheat region imaged withformaldehyde PLIF
high T reaction zone imaged with OH PLIF
CARS line imaging of temperature, species
methane H2Xi OH
JP-8 components formaldehyde
tolueneXi OH
x x
CO
acetylene
CO2
ethylene
Fluorescence: 5 species (Michigan) CARS: 9 species (Gord, Meyer) 27
Chemistrydatareduction
Eachlasershot(someat10Hz,someatkHz)
a) Profileofonespeciesandtemperature(CARSorLIFlineimaging)
JP-8Xi
x, mm
T
b)Simultaneous2-DPLIFimagesofpyrolysislayer,preheat,reactionlayertomeasureresidencetime=thickness/normalvelocity
Forresidencetime=0.1ms
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END
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Events:extinctionwithpoorbacksupport
reactants(black)
noCH=extinction
10kHzCH-OHsimultaneously
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Compare“Events”toDNSofJackieChen,JohnBell
“areaincrease”events:
vortexpassage,flamestretch,extinction,
rollup,merging
“Damkohler diffusion”events
globsofhotgasesconvecting,broadeningthepreheatlayer
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TurbulentBurningVelocity(ST)
previousdataofGulder
lowturbulence=linearvariationofSTextremeturbulence=squarerootdependence
Truemeasuredburningvelocity
Wrinkledarea/timeaveragedarea
AthighReynoldsnumber,wasDamkohlerpredictioncorrect?YES
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“Measurements toDetermine RegimesofPremixedFlames inExtremeTurbulence”,T.Wabel, A.Skiba,J.Temme,J.F.Driscoll
“TurbulentBurningVelocityMeasurements: ExtendedtoExtremeLevelsofTurbulence”T.Wabel,A.Skiba,J.F.Driscoll
“Reaction layervisualization:acomparisonoftwoPLIFtechniquesandadvantagesofkHz-imaging”Skiba,T.Wabel,C.D.Carter,S.Hammack,J.Temme,T.H.Lee,J.F.Driscoll
+twopaperssubmittedforJournalpublication
Formoredetails:seeourrecentpapers
36th Comb.Symp.Seoul:
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1. Events:Merging,extinction,broadening
4. RegimeofContinuousThickenedFlamelets - is largerthanpredictedbyPetersPredicted“Brokenregime”boundary- isnot consistentwithourdata
5. Wemeasuredtheboundary wherepreheatlayersarebroadenedDT >180D*
6. TurbulentburningvelocityatextremeturbulenceagreeswithDamkohler trends
7. PLIFofJP-8,toluene,formaldehyde,OH– carefulselectionofwavelengthsneeded
Conclusions - whathappensatextreme levelsofturbulence?
2.Preheatlayers- becomesverybroadened,Reaction layers– remainthin
3.Stratifiedflamesbecomebrokenanddistributed (butnon-stratifieddonot)
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20-40kHzPulseBurstLaserand10kHzLaser
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Flamelets arenotbroken abovethepredicted“Broken”boundary
1.0
10.0
100.0
1000.0
Lx,0 /δf
u0’/SLPredicted“Broken”boundary
Opensymbols=measured
ThinFlamelets(Gulder)
Presentdata
LaminarWrinkledflames
Dunndata
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1.0
10.0
100.0
1000.0
Lx,0 /δf
u0’/SL
Solidsymbols=MeasuredBroadenedPreheat,ThinReaction
Opensymbols=measured
ThinFlamelets(Gulder)
Presentdata
DT =180D*
LaminarWrinkledflames
MeasuredRegimeDiagram- broadeningboundary
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Goal#3MeasuredRegimes- twomeasuredboundariesdonotagree
Flamelets occurovermuchwiderrangethanwaspredicted
Broadeningofreactionlayersà whenKaPexceedsfivetimespredictedvalue
BroadeningofpreheatLayersà whenDT /D*=180whereDT =u’Lx
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InteractionswithDrs.CamCarter,JimGord AFRL
1. AFRL:KilohertzCHmoviesinHi-Pilot (completed)
2. AFRL:KHzsimultaneousCH-OHinHi-Pilot(completed)
3. ComparedCHtoOverlapmethods (completed)
4.Michigan:SetupJP-8Hi-Pilotflame (completed)
5. AFRLandMichigan:PIVvelocityfield (thiscomingyear)
6. AFRL:RunHi-PilotonJP-8forLineCARS (thiscomingyear)
Michigan:measuredburningvelocities,preheatandoverlap(reaction)layers(completed)
Profilesof14speciesinavaporizedJP-8flame-
canitbedone?
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Extinctionevents- leadtobrokenreactions
CHreactionlayer=thinbrightblueline
OHproducts=broadlightblue
Brokenreactions
darkblue=stratifiedproducts
reactants
Brokenreactions
darkblue=stratifiedproducts
reactants
CH-OHmethodofCamCarter