Consider steady conduction through a large plane wall of thickness ?x = L and surface area A The temperature difference across the wall is ?T = T2 – T1
All modes of heat transfer require the existence of a temperature difference Since for an ideal gas, PV=mRT0 at constant temperature T0, or P=C/V
The rate of heat transfer is given by Fourier's equation: dQ/dt = kA dT/dx Under steady temperature conditions dQ/dt = constant, which may be called q:
where ? is the radiation heat transfer coefficient which is: ? = ( + Heat Equation (used to find the temperature distribution)
conjugate heat transfer/CFD model was run for three cases: (1) constant inner surface temperature, (2) constant inner surface heat flux, and (3) constant
4 sept 2021 · The derivative in equation (6) is merely the slope of the boiling curve and (Rr)-l may be thought of as the effective heat-transfer
with time or time dependence Therefore, the temperature or heat flux remains unchanged with time during steady heat transfer through a medium at any
In this case, the thermal resistance corresponds to electrical resistance, temperature difference corresponds to voltage, and the heat transfer rate corresponds
Heat flux from thermal conduction is also proportional to the temperature gradient across an object and opposite in polarity It varies by a constant k,
Heat flow is a transfer of energy 2 Thermal systems have internal energy related the temperature by a small amount dT with proportionality constant C:
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127942_3FirstLawofThermodynamics_ClosedSystems.pdf
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LawofThermodynamics:ClosedSystems1
TheFirstLawofThermodynamics:ClosedSystems
Thefirstlawofthermodynamicscanbesimplystatedasfollows: duringaninteraction betweenasystemanditssurroundings,theamountofenergygainedbythesystemmust beexactlyequaltotheamountofenergylostbythesurroundings. Aclosedsystemcanexchangeenergywithitssurroundingsthroughheatandwork transfer.Inotherwords,workandheataretheformsthatenergycanbetransferred acrossthesystemboundary. Basedonkinetictheory,heatisdefinedastheenergyassociatedwiththerandom motionsofatomsandmolecules.HeatTransfer Heatisdefinedastheformofenergythatistransferredbetweentwosystemsbyvirtueof atemperaturedifference.
Note:therecannotbeanyheattransferbetweentwo
systemsthatareatthesame temperature. Note:Itisthethermal(internal)energythatcanbestoredinasystem.Heatisaformof energyintransitionandasaresultcanonlybeidentifiedatthe systemboundary. HeathasenergyunitskJ(orBTU).Rateofheattransferistheamountofheattransferred perunittime. Heatisadirectional(orvector)quantity;thus,ithasmagnitude,directionandpointof action.
Notation:
-Q(kJ)amountofheattransfer -Q°(kW)rateofheattransfer(power) -q(kJ/kg)Ͳheattransferperunitmass -q°(kW/kg)Ͳpowerperunitmass
Signconvention
:HeatTransfertoasystemispositive,andheattransferfromasystemis negative.Itmeansanyheattransferthatincreasestheenergyofasystemispositive,and heattransferthatdecreasestheenergyofasystemisnegative.
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Fig.1:Signconvention:positiveiftothesystem,negativeiffromthesystem.
ModesofHeatTransfer
Heatcanbetransferredinthreedifferentmodesconduction,convection,andradiation. Allmodesofheattransferrequiretheexistenceofatemperaturedifference.
Conduction
:isthetransferofenergyfromthemoreenergeticparticlestotheadjacent lessenergeticparticlesasaresultofinteractionsbetweenparticles. Insolids,conductionisduetothecombinationofvibrationsofthemoleculesinalattice andtheenergytransportbyfreeelectrons.
Convection
:isthemodeofenergytransferbetweenasolidsurfaceandtheadjacent liquidorgaswhichisinmotion,anditinvolvesthecombinedeffectsofconductionand fluidmotion(advection). Convectioniscalledforcedifthefluidisforcedtoflowbyexternalmeanssuchasa fanor apump.Itiscalledfreeornaturalifthefluidmotioniscausedbybuoyancyforcesthatare inducedbydensitydifferencesduetothetemperaturevariationinafluid.
Radiation
:istheenergyemittedbymatterintheformofelectromagneticwaves(or photons)asaresultofthechangesintheelectronicconfigurationsoftheatomsor molecules. Work Workistheenergyinteractionbetweenasystemanditssurroundings.Morespecifically, workistheenergytransferassociatedwithforceactingthroughadistance.
Notation:
-W(kJ)amountofworktransfer -W°(kW)power
Q=5kJQ=Ͳ5kJ
HeatinHeatout
System
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-w(kJ/kg)Ͳworkperunitmass -w°(kW/kg)Ͳpowerperunitmass
Signconvention
:workdonebyasystemispositive,andtheworkdoneonasystemis negative.
Fig.2:Signconventionforheatandwork.
Similaritiesbetweenworkandheattransfer:
Botharerecognizedattheboundariesofthesystemastheycrossthem(boundary phenomena). Systems possesenergy,butnotheatorwork(transferphenomena). Bothareassociatedwithaprocess,notastate.Heatorworkhasnomeaningata state. Botharepathfunctions,theirmagnitudesdependonthepathfollowedduringa processaswellastheendstates.
Pathfunctions
:haveinexactdifferentialsdesignatedbysymbolɷ.Properties,onthe otherhand,arepointfunctions whichdependonthestateonly(notonhowasystem reachesthatstate),andtheyhaveexactdifferentials. )W-nor WW not function,Path (Wfunction)(Point 12122
1122
1
WVVVdV
ElectricalWork
Theworkthatisdoneonasystembyelectrons.WhenNcoulombsofelectronsmove throughapotentialdifferenceV,theelectricalworkdoneis:
System
Q
W(+)(Ͳ)
(+) (Ͳ)
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)(Was form rate in the explained becan Which )( e kWVIkJVNW e
Example1:Electricalwork
AwellͲinsulatedelectricalovenisbeingheatedthroughitsheatingelement.Determine whetheritisworkorheatinteraction.Considertwosystems:a)theentireoven(including theheater),andb)onlytheairintheoven(withouttheheater)seeFig3Ͳ3.
Solution:
Theenergycontentoftheovenisincreasedduringthisprocess. a) Theenergytransfertotheovenisnotcausedbyatemperaturedifference betweentheovenandair.Instead,itiscausedbyelectricalenergycrossingthe systemboundaryandthus:thisisaworktransferprocess. b) Thistime,thesystemboundaryincludestheoutersurfaceoftheheaterandwill notcutthroughit.Therefore,noelectronswillbecrossingthesystemboundary. Instead,theenergytransferisaresultofatemperaturedifferencebetweenthe electricalheaterandair,thus:thisisaheattransferprocess.
Fig.3:Schematicforexample1.
Mechanicalwork
Thereareseveralwaysofdoingwork,eachinsomewayrelatedtoaforceactingthrough adistance. )(.kJsFWElectric oven air
Heater
HeaterElectric
oven air
Systemboundary
Systemboundary
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Iftheforceisnotconstant,weneedtointegrate: 2 1 )(.kJdsFW
Therearetworequirementsforaworkinteraction:
theremustbeaforceactingontheboundary theboundarymustmove Therefore,thedisplacementoftheboundarywithoutanyforcetoopposeordrivethis motion(suchasexpansionofagasintoevacuatedspace)isnota workinteraction,W=0. Also,iftherearenodisplacementsoftheboundary,evenifanactingforceexists,there willbenoworktransferW=0(suchasincreasinggaspressureinarigidtank).
MovingBoundaryWork
Theexpansionandcompressionworkisoftencalledmovingboundarywork,orsimply boundarywork. WeanalyzethemovingboundaryworkforaquasiͲequilibriumprocess.Considerthegas enclosedinapistonͲcylinderatinitialPandV.Ifthepistonisallowedtomoveadistance dsin aquasiͲequilibriummanner,thedifferentialworkis:
PdVPAdsdsFW
b . ThequasiͲequilibriumexpansionprocessisshowninFig.4.Onthisdiagram,the differentialareadAundertheprocesscurveinPͲVdiagramisequaltoPdV,whichisthe differentialwork. Note:agascanfollowseveraldifferentpathsfromstate1to2,andeachpath willhavea differentareaunderneathit(workispathdependent). ThenetworkorcycleworkisshowninFig.5.Inacycle,thenetchangeforanyproperties (pointfunctionsorexactdifferentials)iszero.However,thenetworkandheattransfer dependonthecyclepath.
ȴU=ȴP=ȴT=ȴ(anyproperty)=0foracycle
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Fig.4:theareaunderPͲVdiagramrepresentstheboundarywork.
Fig.5:networkdoneduringacycle.
PolytropicProcess
Duringexpansionandcompressionprocessesofrealgases,pressureandvolumeare oftenrelatedbyPV n =C,wherenandCareconstants.Themovingworkforapolytropic processcanbefound: nVPVPdVCVPdVW n polytopic 1 11222
12 1 Since CVPVP nn 2211
.Foranidealgas(PV=mRT)itbecomes: VP W net 12 V 1 V 2
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)(1,1 12 kJnnTTmRW polytropic
Thespecialcasen=1istheisothermalexpansionP
1 V 1 =P 2 V 2 =mRT 0 =C,whichcanbe foundfrom: )(1,ln 12 112
12 1 , kJnVVVPdVVCPdVW isothermalb
Sinceforanidealgas,PV=mRT
0 atconstanttemperatureT 0 ,orP=C/V.
Example2:Polytropicwork
AgasinpistonͲcylinderassemblyundergoesapolytropicexpansion.Theinitialpressureis
3bar,theinitialvolumeis0.1m
3 ,andthefinalvolumeis0.2m 3 .Determinetheworkfor theprocess,inkJ,ifa)n=1.5,b)n=1.0,andc)n=0.
Solution:
Assumethati)thegasisaclosedsystem,ii)themovingboundaryisonlyworkmode,and iii)theexpansionispolytropic. a)n=1.5 2 1 1122
1 V V nVPVPPdVW
WeneedP
2 thatcanbefoundfrom nn VPVP 2211
: barbarVVPP n
06.12.01.03
5.1 2 1 12 kJmNkJ barmNmbarW6.17.101 1/10
5.111.032.006.1
3253
b)n=1,thepressurevolumerelationshipisPV=constant.Theworkis: kJmNkJ barmNmbarWVVVPPdVW
79.201.02.0ln.101
1/101.03ln
325
312
112
1 c)Forn=0,thepressureͲvolumerelationreducestoP=constant(isobaricprocess)andthe integralbecomeW=P(V 2 ͲV 1 ). Substitutingvaluesandconvertingunitsasabove,W=30kJ.
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Springwork
Forlinearelasticsprings,thedisplacementxisproportionaltotheforceapplied: xkF s wherek s isthespringconstantandhastheunitkN/m.Thedisplacementxismeasured fromtheundisturbedpositionofthespring.Thespringworkis: )(21 2 12 2 kJxxkW sspring Note:theworkdoneonaspringequalstheenergystoredinthespring.
NonͲmechanicalformsofwork
NonͲmechanicalformsofworkcanbetreatedinasimilarmannertomechanicalwork. SpecifyageneralizedforceFactinginthedirectionofageneralizeddisplacementx,the worktransferassociatedwiththedisplacementdxis: dxFW.
Example3:Mechanicalwork
Calculatetheworktransferinthefollowingprocess:
Fig.6:SchematicPͲVdiagramforExample3.
Solution:
Process1Ͳ2isanexpansion(V
2 >V 1 )andthesystemisdoingwork(W 12 >0),thus: W 12 =P 1 (V 2 ͲV 1 )+[0.5(P 1 +P 2 )-P 1 ](V 2 -V 1 ) =(V 2 -V 1 )(P 1 +P 2 )/2
Process2Ͳ3isanisometricprocess(constantvolumeV
3 =V 2 ),soW 23
=0
Process3Ͳ1isacompression(V
3 >V 1 ),workisdoneonthesystem,(W 31
<0) 12 3 V V 2 V 1 P 1 P 2 P
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W 31
=ͲP 1 (V 2 -V 1 ) W cycle =W net =W 12 +W 23
+W 31
=(V 2 -V 1 )(P 2 -P 1 )/2 NotethatinacycleȴU=ȴP=ȴT=ȴ(anyproperty)=0
FirstLawofThermodynamics
Firstlaw,ortheconservationofenergyprinciple,statesthatenergycanbeneithercreated nordestroyed;itcanonlychangeforms.
Thefirstlawcannotbeprovedmathematically,
itisbasedonexperimentalobservations, i.e.,therearenoprocessinthenaturethatviolatesthefirstlaw. Thefirstlawforaclosedsystemorafixedmassmaybeexpressedas: netenergytransferto(orfrom) thesystemasheatandwork=netincrease(or decrease)inthetotal energyofthesystem
Q-W=ȴE(kJ)
where
Q=netheattransfer(=ɇQ
in -ɇQ out )
W=networkdoneinallforms(=ɇW
in -ɇW out )
ȴE=netchangeintotalenergy(=E
2 -E 1 ) Thechangeintotalenergyofasystemduringaprocesscanbeexpressedasthesumof thechangesinitsinternal,kinetic,andpotentialenergies:
ȴE=ȴU+ȴKE+ȴPE(kJ)
122
12 212
21
zzmgPEVVmKEuumU ' Note:forstationarysystemsȴPE=ȴKE=0,thefirstlawreducesto
Q-W=ȴU
ThefirstlawcanbewrittenonaunitͲmassbasis:
q-w=ȴe(kJ/kg) orindifferentialform:
ɷQ-ɷW=dU(kJ)
ɷq-ɷW=du
(kJ/kg) orintherateform:
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Q°-W°=dE/dt(kW) Foracyclicprocess,theinitialandfinalstatesareidentical,thusȴE=0.Thefirstlaw becomes:
Q-W=0(kJ)
Note:fromthefirstlawpointofview,thereisnodifferencebetweenheattransferand work,theyare bothenergyinteractions.Butfromthesecondlawpointofview,heatand workareverydifferent.
Example4:Fistlaw
AiriscontainedinaverticalpistonͲcylinderassemblyfittedwithanelectricalresistor.The atmosphericpressureis100kPaandpistonhasamassof50kg andafaceareaof0.1m 2 . Electriccurrentpassesthroughtheresistor,andthevolumeofairslowlyincreasesby
0.045m
3 .Themassoftheairis0.3kganditsspecificenergyincreasesby42.2kJ/kg. Assumetheassembly(includingthepiston)isinsulatedandneglectthefrictionbetween thecylinderandpiston,g=9.8m/s 2 .Determinetheheattransferfromtheresistortoair forasystemconsistinga)theairalone,b)theairandthepiston.
Fig.7:Schematicforproblem4.
Assumptions:
Twoclosedsystemsareunderconsideration,asshowninschematic. Theonlyheattransferisfromthe resistortotheair.ȴKE=ȴPE=0(forair) Theinternalenergyofthepistonisnotaffectedbytheheattransfer. a)Takingtheairasthesystem, (ȴKE+ȴPE+ȴU) air =Q-W
AirPistonAirPiston
System
boundary partb
System
boundary parta
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Q=W+ȴU air Forthissystemworkisdoneatthebottomofthepiston.Theworkdonebythesystemis (atconstantpressure): 2 1 12V V
VVPPdVW
Thepressureactingontheaircanbefoundfrom:
PA piston =m piston g+P atm A piston kPakPaPakPa mNPa msmkgPP AgmP atm
91.10410010001
/11
1.0/81.950
222pistonpiston
Thus,theworkis
W=(104.91kPa)(0.045m
3 )=4.721kJ
WithȴU
air =m air ȴu air ,theheattransferis Q=W+m air ȴu air =4.721kJ+(0.3kg)(42.2kJ/kg)=17.38kJ b)systemconsistingtheairandthepiston.Thefirstlawbecomes: (ȴKE+ȴPE+ȴU) air +(ȴKE+ȴPE+ȴU) piston =Q-W where(ȴKE=ȴPE) air =0and(ȴKE=ȴU) piston =0.Thus,itsimplifiesto: (ȴU) air +(ȴPE) piston =Q-W Forthissystem,workisdoneatthetopofthepistonandpressureistheatmospheric pressure.Theworkbecomes W=P atm
ȴV=(100kPa)(0.045m
3 )=4.5kJ Theelevationchangerequiredtoevaluatethepotentialenergychangeofthepistoncan befoundfromthevolumechange:
ȴz=ȴV/A
piston =0.045m 3 /0.1m 2 =0.45m (ȴPE) piston =m piston gȴz=(50kg)(9.81m/s 2 )(0.45m)=220.73J=0.221kJ
Q=W+(ȴPE)
piston +m air ȴu air
Q=4.5kJ+0.221kJ+(0.3kg)(42.2kJ/kg)=17.38kJ
Notethattheheattransferisidenticalinbothsystems.
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SpecificHeats
Thespecificheatisdefinedastheenergyrequiredtoraisethetemperatureofaunitmass ofasubstancebyonedegree.Therearetwokindsofspecificheats: specificheatatconstantvolume,Cv(theenergyrequiredwhenthevolumeis maintainedconstant) specificheatatconstant pressure,C p (theenergyrequiredwhenthepressureis maintainedconstant)
ThespecificheatatconstantpressureC
p isalwayshigherthanC v becauseatconstant pressurethesystemisallowedtoexpandandenergyforthisexpansionmustalsobe suppliedtothesystem. Let'sconsiderastationaryclosedsystemundergoingaconstantͲvolumeprocess(w b =0).
Applyingthefirstlawinthedifferentialform:
ɷq-ɷw=du
atconstantvolume(nowork)andbyusingthedefinitionofC v ,onecanwrite: vvv
TuCordudTC
Similarly,anexpressionforthespecificheatatconstantpressureCpcanbefound.From thefirstlaw,foraconstantpressureprocess(w b +ȴu=ȴh).Ityields: pp ThC specificheats(bothC v andC p )arepropertiesandthereforeindependentofthe typeofprocesses. C v isrelatedtothechangesininternalenergyu,andC p tothechangesinenthalpy, h.
Itwouldbemoreappropriatetodefine:C
v isthechangeinspecificinternalenergyper unitchangeintemperatureatconstantvolume.C p isthechangeinspecificenthalpyper unitchangeintemperatureatconstantpressure.
Specificheatsforidealgases
Ithasbeenshownmathematicallyandexperimentallythattheinternalenergyisa functionoftemperatureonly. u=u(T)
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Usingthedefinitionofenthalpy(h=u+Pv)andtheidealgasequationofstate(Pv=RT), wehave: h=u+RT
SinceRisaconstantanduisafunctionofTonly:
h=h(T)
Therefore,atagiventemperature,
u,h,C v andC p ofanidealgaswillhavefixedvalues regardlessofthespecificvolumeorpressure.Foranidealgas,wehave: dTTCdhdTTCdu pv Thechangesininternalenergyorenthalpyforanidealgasduringaprocessare determinedbyintegrating: )/()/( 2 1 122
1 12 kgkJdTTChhhkgkJdTTCuuu pv Aslowpressures,allrealgasesapproachidealͲgasbehavior,andthereforetheirspecific heatsdependontemperatureonly.Thespecificheatsofrealgasesatlowpressuresare calledidealͲgasspecificheats(orzeroͲpressurespecificheats)andareoftendenotedby C p0 andC v0 .Tocarryouttheaboveintegrations,weneedtoknowC v (T)andC p (T).These areavailablefromavarietyofsources: TableAͲ2a:forvariousmaterialsatafixedtemperatureofT=300K TableAͲ2b:variousgasesoverarangeoftemperatures250чTч1000K TableAͲ2c:variouscommongasesintheform ofathirdorderpolynomial
Foranidealgas,wecanwrite:
vp
CCRdTdu
dTdhRTuThRT Theratioofspecificheatsiscalledthespecificheatratiok=C p /C v : varieswithtemperature,butthisvariationisverymild. formonatomicgases,itsvalueisessentiallyconstantat1.67. Manydiatomicgases,includingair,haveaspecificheatratioofabout1.4atroom temperature.
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Specificheatsforsolidsandliquids
Asubstancewhosespecificvolume(ordensity)isconstantiscalledincompressible substance.Thespecificvolumesofsolidsandliquids(whichcanbeassumedas incompressiblesubstances)essentiallyremainconstantduringaprocess. Theconstantvolumeassumptionmeansthatthevolumework(boundarywork)is negligiblecomparedwithotherforms ofenergy.Asaresult,itcanbeshownthatthe constantͲvolumeandconstantͲpressurespecificheatsareidenticalforincompressible substances: C p =C v =C Specificheatsofincompressiblesubstancesareonlyafunctionoftemperature,
C=C(T)
Thechangeofinternalenergybetweenstate1and2canbeobtainedbyintegration: )/( 2 1 12 kgkJdTTCuuu Forsmalltemperatureintervals,aCataveragedtemperaturecanbeusedandtreatedas aconstant,yielding: 12 TTCu ave Theenthalpychangeofincompressiblesubstancecanbedeterminedfromthedefinition ofenthalpy(h=u+Pv) h 2 -h 1 =(u 2 -u 1 )+v(P 2 -P 1 )
ȴh=ȴu+vȴP(kJ/kg)
ThetermvȴPisoftensmallandcanbeneglected,soȴh=ȴu.
Example5:Specificheatandfirstlaw
Twotanksareconnectedbyavalve.Onetankcontains2kgofCO 2 at77°Cand0.7bar. Theothertankhas8kgofthesamegasat27°Cand1.2bar.Thevalveisopenedand gasesareallowedtomixwhilereceivingenergybyheattransferfromthesurroundings. Thefinalequilibriumtemperatureis42°C.Usingidealgasmodel,determine a)thefinal equilibriumpressureb)theheattransferfortheprocess.
Assumptions:
ThetotalamountofCO 2 remainsconstant(closedsystem). IdealgaswithconstantC v . Theinitialandfinalstatesinthetanksareequilibrium.Noworktransfer.
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Thefinalpressurecanbefoundfromidealgasequationofstate: 2121
21
VVRTmm
VVRTmP
fft f
Fortank1and2,wecanwrite:V
1 =m 1 RT 1 /P 1 andV 2 =m 2 RT 2 /P 2 .Thus,thefinalpressure, P f becomes: bar barKkg barKkgKkgPPTm
PTmTmm
P RTm
PRTmRTmmP
fff f 05.1
2.13008
7.0350231510
222
11121
2 22
11121
b)Theheattransfercanbefoundfromanenergybalance:
ȴU=Q-W
WithW=0,
Q=U f -U i whereinitialinternalenergyis:U i =m 1 u(T 1 )+m 2 u(T 2 )
Thefinalinternalenergyis:U
f =(m 1 +m 2 )u(T f )
Theenergybalancebecomes:
Q=m 1 [u(T f )-u(T 1 )]+m 2 [u(T f )-u(T 2 )]
SincethespecificheatC
v isconstant Q=m 1 C v [T f -T 1 ]+m 2 C v [T f -T 2 ] kJKKKkgkJkgKKKkgkJkgQ25.37300315.745.08350315.745.02 Theplussignindicatesthattheheattransferisintothesystem. CO 2
8kg,27C,1.2barCO
2
2kg,77C,0.7bar
Valve