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191KKU Res. J. 2013; 18(2)
Combined Convective and Radiative Heat Transfer on Transpiration Cooling System in Al-Co Open-celled Foam having PPI of 20
Pipatana Amatachaya,1 Bundit Krittacom1,* and Rapeepong Peamsuwan2
1 Development In Technology Of Porous Materials Research Laboratory (DITO-Lab), Department of Mechanical Engineering, Faculty of Engineering and Architecture,2 Department of Applied Physics, Faculty of Sciences and Liberal Arts, Rajamangala University of Technology Isan (RMUTI), 744 Suranarai Road, Maung, Nakhonratchasima, 30000, THAILAND, Tel: +664-423-3073, Fax: +664-423-3074* Correspondent author: [email protected] and [email protected]
Abstract
One-dimensionaltranspirationcoolingsysteminopen-celledfoamhasbeenconductedexperimentally
and numerically to investigate the heat transfer characteristics of combined convection and radiation.The
Alumina–Cordierite (Al-Co) open-cell foamhaving porosity of 0.875 and pores per inch (PPI) of 20was
employed.Theuppersurfaceofporousplatewasheatedbytheheatfluxofincomingradiation(qRx,f)varyingfrom
0.97-16.59kW/m2whereasairinjectionvelocity(uf)fedintothelowersurfacewasvariedfrom0.364-1.274
m/s,andwasthenrearrangedasReynoldsnumber(Re).Forthereportoftheresultsinthepresentstudy,two
efficienciesincludingoftemperature(hT)andconversionefficiency(h
C)werepresented.Theh
Tincreasedrapidly
withtheairinjectionvelocity(Re).ItwasthensaturatedandhadaconstantvalueatRehigherthan15.Forthe
resultofhC,itwasdecreasedslightlywithincreasingofq
Rx,fandu
f(Re).Thenumericalpredictionsalsoagreed
withexperimentaldataverywell.
Keywords: Open-cellfoam,Radiation,Transpirationcooling,Reynoldsnumber
KKU Res. J. 2013; 18(2): 191-199http : //resjournal.kku.ac.th
192 KKU Res. J. 2013; 18(2)
1. Introduction
Transpirationcoolingoreffusioncooling(1)
is theprocessof injectingafluid (Air) intoaporous
materialwhichcanbeservedasaveryefficientcooling
methodforprotectingsolidsurfaces thatareexposed
tohigh-heat-flux,high-temperaturefromenvironments
suchasinhypersonicvehiclecombustors,rocketnozzle,
gasturbineblades,andthestructureofre-entryaerospace
vehicles(1–5).Theperformanceofthiscoolingsystem
is governed by several parameters such as radiative
propertiesofporousmedia,thevolumetricheattransfer
coefficientbetweenthesolidphaseandfluid,fluidvelocity
andirradiation.Thus,theknowledgeofparametersfor
thedesignoftranspiration-cooleddevicesisclassified
intotwomaingroupsincludingthephenomenaoffluid
flowandheattransferprocesswithintheporousplate.
Sofaranumberofexperimentalworks(6–8)
andnumericalstudies(9–12)havebeenconductedon
transpirationcoolingsystem.However,mostofprevious
studiesweremainlyintendedtodeterminetheeffects
of convectionmode.Therewere only a few studies
have taken into account the radiativeheat transfer in
thetranspirationcoolingsystem.Recently,Jiangetal.
(13)andKamiutoetal.(14)investigatedexperimentally
andanalyticallytoextendthevalidationofnumerical
model.Jiangetal.(13)foundthatthenumericalresults
correspondedwellwiththeexperimentaldataincluding
thesurfacetemperatureandheattransfercoefficients.
However, theirwork still focused on the effects of
convectiveheattransfer.Radiationmodewasconcerned
intheinvestigationofKamiutoetal.(14).Theyreported
thattheagreementbetweentheoreticalpredictionand
experimentalresultswasacceptable.AlthoughKamiuto
andco-worker(14)regardedtheradiationmodeinthe
transpirationcoolingsystem,thetheoreticalresultwas
moreemphasizedandthereexistthedifferencebetween
theoryandexperiment.
BasedontheworkofKamiutoetal.(14),the
presentresearchaimstofurtherexperimentandanalyze
theheat transferphenomenaas combinedconvection
and radiation in the transpiration cooling system
usingopen-cellularporousmaterial.Alumina-Cordierite
(Al-Co)havingPPIof20isadoptedowingtothisAl-Co
hasahigherporosityresultingtoahigherefficientof
heattransferandiswidelyusedasthermalinsulationof
industry(15).Obtainablequantitiessuchastemperature
atthesurfacesandwithintheporousplate,fortheoretical
results,arepresentedandcomparisonwithexperimental
dataisalsoreported.Atipfordesignisrecommended.
2. Nomenclature
Cf, isobaricspecificheatcapacity(J•kg-1•K-1)
DC anormalcelldiameter(m)
DP equivalentstrutdiameter(m)
asymmetricfactorofscatteringphasefunction
G incidentradiation(W/m2)
hv volumetric heat transfer coefficient betweengas
andsolidphases(W•m-3•K-1)
kf thermalconductivityofagasphase(W•m-2•K-1)
ks thermalconductivityofasolidphase(W•m-2•K-1)
qRx netradiativeheatfluxinxdirection(W/m2)
Tf temperatureofagasphase(oC)
TR radiationblackbodytemperature(K)
Ts temperatureofasolidphase(oC)
T∞ ambienttemperature(K)
uf airflowvelocity(m/s)
w dimensionlesswidthofastrutwithasquarecross
section(m)
x coordinateintheflowdirection(m)
193KKU Res. J. 2013; 18(2)
Greek Symbols
β scaledextinctioncoefficient(m-1)
f porosity
hT temperatureefficiency
hC conversionefficiency
rf densityofagasphaseorair(kg/m3)
s Stefan–Boltzmann constant (=5.67×10-8
W•m-2•K-4)
t opticalthickness
w scaledalbedo
3. Theoretical Analysis
3.1 Mathematical Model
Thepresentmodelofatranspirationcooling
system is shown in Fig. 1. The assumptions of the
numericalmodelaresimilartothoseofKamiutoetal.
(14).However,somemodificationwasmadetoimprove
the accurate prediction. The following assumptions
were introduced for this analysis as follows: 1)An
open-cellular porous plate of thickness x0 is placed
horizontally; 2)The front surface of porous plate is
uniformly irradiated by blackbody radiation at an
equivalenttemperatureTR(K),whilethebacksurface
is subject to uniformblackbody radiation at an inlet
air temperature; 3)A low-temperature air is injected
throughthebacksurfaceofporousplateandisassumed
tobenon-radiating;4)Theporousmediumisgrayand
is capable of emitting, absorbing and anisotropically
scattering thermal radiation; 5)The porousmedium
isnon-catalytic;6)Thephysicalpropertiesdependon
temperaturedifferedfromKamiuto’swork(14)thatthe
physicalpropertiesofhiswork(14)didnotdependon
temperature;7)Theheattransferwithintheporousplate
isinanone-dimensionalsteady-state;8)Thebehavior
of air flowwithin porous plate is under local and
non-thermalequilibriumcondition.
Figure 1. The theoreticalmodel and coordinate of a
transpirationcoolingsystem.
Under these assumptions, the continuity
equationisgivenby:
(1)
Thegoverningenergyequations for thegas
andthesolidphases(porousplate)maybewrittenas
follows:
(2)
(3)
(4)
Fourphysicalproperties,i.e.,f,β,hvandw
fromEq.(2)to(4)weresummarizedbyKrittacom(16)
andwerebrieflyrecalledasfollowing:
(5)
(6)
194 KKU Res. J. 2013; 18(2)
(7)
(8)
(9)
(10)
TheGrepresentstheincidentradiationandqRx
denotesasthenetradiativeheatfluxintheflowdirection.
Thesequantitiescanbedeterminedfromtheequationof
radiativetransfer.Oncetheradiationfieldisspecified,
thequantitiesGandqRxcanbereadilyevaluated.The
radiativeheatequationofthepresentresearchissolved
bytheP1approximation(17)andiswrittenas:
(11)
(12)
Theboundaryconditionsfor(2),(3),(4),(11)
and(12)aregivenasfollows:
(13)
(14)
3.2 Numerical Method
Forconvenienceofcalculations,thegoverning
equations and associated boundary equations are
transformed into dimensionless forms, and then the
dimensionlessequationsaresolvednumericallyusing
animplicitdifferencemethod.Forsolvingtheequation
oftransferwiththeP1equations,andcalculationsofthe
TfandT
s,theporousplateisdividedinto300equally
spaced increments,whereas the optical thickness is
dividedinto600equallyspacedincrements.Toobtain
thesolutionsofTfandT
s,Gorq
Rxarefirstdetermined
basedonantheassumptionoftemperatureprofile,and
thenthequantitiesofGandqRxaregainedbysolving
equation of transfer or theP1 equations at staggered
latticepoints(17).OnceGisobtained,thefinitedifference
equationsforTfandT
scanbesolvedreadilybyGaussian
elimination.Thereafter,thederivedsolutionsofTfand
TsaresubstitutedintotheequationoftransferortheP
1
equationsandtheenergyequationstogetnewsolutions
of these quantities; similar calculations are repeated
until the following convergence criterion is satisfied:
Here,Q representsTf, T
s,
Gor qRx, and n is time interval of calculation.After
obtainingtheTf,T
sandG,twoefficiencies,temperature
efficiency (hT) and conversion efficiency (h
C) are
evaluatedasfollows:
(15)
(16)
ThephysicalmeaningofhTistheindicating
howclosethemeantemperatureofaporousheatplate
tothatofinletairandhCisregardedastheabilityof
porousmaterial in transferring energyby convection
afterabsorbedfromheatradiation,
4. Experimental Apparatus and
Procedure
4.1 Experimental Apparatus
Figure 2 shows a schematic diagramof the
presentexperimentalapparatus.Theexperimentalset-up
wasconstructedsimilartothatofKamiutoetal.(14),
195KKU Res. J. 2013; 18(2)
butthedouble-tubeheatexchangerwasinstalledatthe
airinlettokeepairtemperatureat25–30oCwhenit
reachedthebacksurfaceoftheporousplate.Therefore,
the present transpiration cooling systemconsisted of
4 sections includingheat exchanger, inlet air, porous
medium,andradiationsection.Airfromablowerthat
wasusedas the transpirationgaswasblown through
theheat-exchangerandmeasuredtheflowrateusinga
rotameter.Theairwasthenflowedupwardthrougha
stainlesspipe(0.01minnerdiameterand0.6mhigh)
insteadofacrylicpipeasinKamiutoetal.(14).Aporous
platemadeofAlumina-Cordierite(Al-Co)wasplacedon
thetopofthestainlesspipe.Thephysicalcharacteristics
oftheexaminedporousplateweresummarizedintable
1.Four250-Winfraredlampswerealignedabovethe
porousplatetoirradiatetheheatintotheuppersurface
oftheplate.Theamountofradiantenergywasmeasured
using heat flux sensormanufactured byHukesflux
Thermal Sensor,modelHFP01-05.The intensity of
theinfraredlampswasregulatedmanuallyfrom50V
to250V;thustheradiativeheatfluxwasvariedfrom
0.97to16.59kW/m2.
Figure 2.Schematicdiagramoftheexperimentalapparatus.
Table 1. PhysicalcharacteristicsofaAlumina-Cordierite(Al-Co)open-cellularporousmaterial
Coefficients Quantities
Porosity f 0.875
Poresperinches PPI 20
Thickness x 0.0103m
Extinctioncoefficient β 365.89m-1
Opticalthickness t 3.77
196 KKU Res. J. 2013; 18(2)
4.2 Experimental Procedure
Theprocedureoftheexperimentaloperation
of thepresentcooling system isalso similar to those
ofKamiuto et al. (14).After the infrared lamps are
switchedon,ittakesabout40-60minutestoattaina
steady-stateofthetemperaturesoftheporousplate.Six
type-Kthermocoupleelementsof0.0003mindiameter
are adhered on the upper and lower surfaces of the
porousplatebydividingasthreeforeachsurface.Inlet
andoutletair temperaturearemeasuredusingtype-K
sheathedthermocouple.Theairvelocityisvariedfrom
0.364-1.274m/s.
5. Results and Discussion
5.1 Effects of Air Flow Velocity (uf) on
Temperature Profile
Figure3presentedthetheoreticalresultsofthe
temperatureprofilesofthesolid(Ts)andthegasphases
(Tf)insidetheAl-Coporousplate,underthecondition
ofirradiatedheatfluxqRx,f=12.48kW/m2.Asseenfirst
inFig.3(a),themeasuredmeansurfacetemperaturesof
thefrontandbackporousplateareindicatedbysymbols,
whilethecalculatedresultsforthesolidphase(Ts) is
presented using the lines.The trend ofTs increased
alongtheporouslengthbecausetheincidentradiation
fromtheinfraredlampswasemitteddowntothefront
surface.For afixedpositionof the thickness (x), the
temperatureprofilesofTfdeceasedastheairvelocity
(uf)increasedowingtotheeffectsofahigherconvective
heat transfer (10).Agreementbetween theprediction
calculatedbybasingontheP1equationintheradiative
transferequation(RTE)andtheexperimentalresultsat
theback(x=0mm)andthefrontsurface(x=10mm)
weresatisfactory.InFig.3(b),thetemperatureprofiles
ofTfshowedthetrendsimilartoT
scase;itincreased
alongtheporouslengthanddeceasedwithufincreasing.
ForcomparisonofTsandT
f,itwasobviouslyfoundthat
Tswashigher thanT
fbecause thesolidporousphase
receivedtheradiationheatfluxdirectlyandthen,next
step, the energy absorbed by porousmaterial was
transferredtotheairsuppliedintosystem(18).
Figure 3. Profiles of Ts and T
f within the Al-Co
open-cellularplatefortheeffectofuf
5.2 Effects of Heat Flux on Temperature
Profile
Figure4showedthetheoreticalresultsofthe
temperatureprofileofthesolid(Ts)andthegasphases
(Tf)insidetheAl-Coporousplate,underthecondition
ofairflowvelocity(uf)of0.848m/s.AsseenfirstinFig.
4(a),thetrendofTsincreasedalongtheporouslength
duetoincidentradiationfromtheinfraredlamps.For
afixedpositionofthicknessx,thetemperatureprofiles
197KKU Res. J. 2013; 18(2)
ofTsincreasedwithradiativeheatflux(q
Rx,f)owingto
porousmediumabsorbedahigherradiantenergyfrom
theinfraredlamps.Agreementbetweentheprediction
basedon theP1model ofRTEand the experimental
resultsattheback(x=0mm)andthefrontsurface(x=
10mm)weresatisfactory.InFig.4(b),thetemperature
profilesofTfexpressedthetrendsimilartoT
scase;it
increased along the porous length gradually and
increasedwithqRx,f.ForcomparisonofT
sandT
f,itwas
obviouslyfoundthatTswashigherthanT
fwhichwas
describedbythesamereasonofFig.3(b).
Figure 4. Profiles of Ts and T
f within the Al-Co
open-cellularplatefortheeffectofqRx,f
5.3 The Temperature Efficiency (hT)
Figure5showsvariationsinthetemperature
efficiencyhTagainstReynolsnumber(Re).Inthisstudy,
Rerepresentstheairflowvelocitywhichisdefinedby
usingrfu
fD
s/m
f,wherem
fisviscosityofagasphase
(Pa•s), andDs is theequivalent strutdiameter (m)as
describedinKrittacom(15).Theexperimentalresults
areshownusingsymbols,whilethenumericalresults
areindicatedbyusingthelines.Thefiguredepictedthat
thehTincreasedrapidlywithReandthenasymptotic
toaconstantvaluefortheRehigherthan15.However,
atafixedRe,thehTdecreasedwiththeincreaseofthe
incidentradiationduetoahigherdifferenceofanaverage
temperatureofporousplateandairtemperaturefedto
systemwasobtained.For theRehigher than15, the
values ofhTwere greater than 95 percentage. This
indicatedthattheaveragetemperatureoftheporousplate
wasveryclosetotheaverageheatshieldtemperature
andinletairtemperature.Agreementbetweentheoryand
experimentwasacceptablewhichindicatedthevalidity
ofthepresentnumericalmodel.
Figure 5. Temperature efficiency (hT) of theAl-Co
open-cellularporousplate
5.4 The Conversion Efficiency (hC)
Figure6showsvariations in theconversion
efficiencyhC againstRe. The results demonstrated
that thehC increased slightlywithRe inwhich the
hCvalueswerevariedintherangeof40%to60%.But
the value ofhCwas asymptotic to a constant value
fortheRehigherthan15.ForafixedvalueofRe,hC
198 KKU Res. J. 2013; 18(2)
increasedwithincidentradiation(qRx,f)becausetheporous
mediaabsorbedenergyfromahigherheatfluxandthen
transferred via convection through the cooled-air
flow.Thus,theabilityoftransferringenergyofAl-Co
open-cellularporousplatebyconvectionafterabsorbing
heat radiation decreasedwith the increasing of heat
flux.Agreementbetween theory and experimentwas
acceptable.
Figure 6.Conversion efficiency (hC) of theAl-Co
open-cellularporousplate
6. Conclusion
Themajorconclusionsthatcanbedrawnfrom
thepresentstudyaresummarizedasfollows:
1) The temperatureprofilesofgas (Tf)and
solid(Ts)phasedeceasedasairinjectionvelocity(u
f)
increasedbecauseoftheeffectsofahigherconvective
heattransfer,whereastheprofilesofbothtemperature
increasedwith incident radiation (qRx,f) owing to the
effectsofhigherradiantenergy.
2) Thetemperatureefficiency(hT)increased
rapidlywithReandthenasymptotictoaconstantvalue
fortheRehigherthan15butthehTdecreasedwiththe
increaseoftheqRx,f.
3) Theconversionefficiency(hC)ofaAl-Co
open-celledfoamincreasedslightlywithReandandthen
asymptotictoaconstantvaluefortheRehigherthan15
aswellasthevalueofhCwasgovernedbyheatflux
(qRx,f).
4) Agreementbetweenthepredictedresults
based on P1 equations and experimental data was
acceptable, thereby the validity of theoreticalmodel
wasconfirmed.
Suggestions and a Designed Tip
Incoming radiation from a radiative
environment can be almost completely protected as
longastheReoftheopen-cellularplatewasabout15
orhigher.Asaresult,thetranspirationcoolingsystem
asusedinthepresentopen-cellularporousplateshould
bedesignedfortheRe=15.
7. Acknowledgement
WearegratefultotheRajamangalaUniversity
ofTechnology Isan (RMUTI) for the research fund.
WealsoexpressourthankstoMr.JeerasakKamluang,
Miss Pensiri Thikumrum,Mr.KriengkaiDastaisong,
Mr.KritsadaPoohbunyaandMr.ChutchaiKrongpeug,
studentswho is themembers of theDevelopment in
TechnologyofPorousMaterialsResearchLaboratory
(DITO-Lab), for their assistance in performing some
partoftheexperiments.
8. References
(1) GrootenhuisP.Themechanismandapplicationof
effusioncooling.JournaloftheRoyalAeronautic
Society.1959;63:pp.73–89.
(2) Choi SH, Scotti SJ, SongKD and Ries H.
Transpiring cooling of a scram-jet engine
combustionchamber:NASA(US);1997.8p.
ReportNo.:NASAAIAAA-97-2576.
(3) GlassDE,DilleyADandKellyHN.Numerical
analysis of convection/ transpiration cooling.
199KKU Res. J. 2013; 18(2)
AIAAJSpacecraftRockets.2001;38(1):15–20.
(4) Bayley FJ andTurnerAB.The heat transfer
performance of porous gas turbine blades.
AeronauticalJournal.1968;72:1087–1094.
(5) BayleyFJandTurnerAB.Transpirationcooled
turbines. JournalProceedingof the Institution
ofMechanicalEngineeringwithturbine.1970;
185(1):943-956.
(6) DuwezPandWheelerHL.Experimentalstudyof
coolingbyinjectionofafluidthroughaporous
material.JournalofAeronauticalSciences.1948;
15:509–521.
(7) Andrews GE and Asere A. Transpiration
coolingofgasturbinecombustionchamberwalls.
InstituteofChemicalEngineeringSymposium
Series.1984;86:1047-1056.
(8) FuX,ViskantaR andGore JP.Measurement
and correlation of volumetric heat transfer
coefficients.ExperimentalandThermalandFluid
Science.1988;17(4):285-293.
(9) KubotaH.Thermalresponseofatranspiration-
cooled system in a radiative and convective
Environment.TransactionoftheASME:Journal
ofHeatTransfer.1977;99:628–633.
(10) Eckert ERG and ChoHH. Transition from
transpiration tofilm cooling. Int JHeatMass
Transfer.1994;37(suppl1):3–8.
(11) Wolfersdorf JV. Effect of coolant side heat
transfer on transpiration.HeatMassTransfer.
2005;41:.327-337.
(12) AndohYHandLipsB.Predictionofporouswalls
thermalprotectionbyeffusionor transpiration
cooling. An analytical approach. Applied
ThermalEnergy.2003;23(15):1947-1958.
(13) Jiang P-X, Yu L, Sun J-G and Wang J.
Experimental and numerical investigation of
convectionheattransferintranspirationcooling.
AppliedThermalEngineering.2004;24(8-9):
1271-1289.
(14) Kamiuto K. Thermal characteristics of
transpirationcoolingsystemusingopen-cellular
porousmaterials in a radiative environment.
2005;7:58-96.
(15) OgushiT,ChibaH,TaneMandNakajimaH.
CellularandPorousMaterials.OchsnerA,Murch
GEandLemonMJS,editor.Wiley-VCHVerlag
GmbH&Co.KGaA;2008.
(16) KrittacomB.StudiesonThermalCharacteristics
ofOpen-CellularPorousBurners[Ph.D.Thesis].
Oita,Japan:OitaUniversity;2009.
(17) KamiutoK,SaitoSandItoK.Numericalmodel
for combined conductive and radiative heat
transferinannularpackedbeds.NumericalHeat
Transfer,PartA.1993;23:433-443.
(18) KrittacomB andAmatachayaP.Comparison
of radiative heat transfer equation in porous
materials solving by the equation of formal
solution and the P1 approximation equation.
EngineeringJournalofSiamUniversity.2008;
9(1):20-30.Thai.