4 first law analysis (open systems)
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Chapter#4FirstLawAnalysis(opensystems)
Controlvolumeanalysis
Massbalanceequation
Energybalanceequation
Steadystateflowprocesses
Charginganddischargingofcylinders
ControlVolumeAnalysis Focus on a specified region in space through which material
flows continuously in and out
(e.g. turbines, compressors, pumps, heat exchangers)
Heat and work interaction across control surface
Control volume need not be constant in volume and shapeand may undergo configuration change.
Most often, we deal with control volumes that are of fixedshape and size.
To analyze continuous flow processes
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Massanalysisforopensystems
Let us consider a control volume,
let dmi= mass entering in control volume during time intervaldt
dme= mass leaving in time dt
m(t) = mass inside control volume at time t
m(t + dt) = mass inside control volume at time (t + dt)
Writin law of conservation of mass
m (t + dt) = m(t) + dmidme
m(t+dt) m(t)=dmi dme
Dividebydt,
[m(t+dt) m(t)]/dt =dmi/dt dme /dt
In imit t0;dm/dt =dmi/dt dme /dt
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Ifcontrolvolumehasmanyinletportandexitports,
Rateofmassaccumulation=
Netrateofmassin Netrateofmassout
(Equationofcontinuity)
Particularly,forsteadystateprocess,
dm/dt =0,
m=constant
andtotalmassrate(in)=Totalmassrate(out)
Energyanalysisforopensystems Considerfollowinganopensystem(e.g.steamturbine),
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Let m(t) = total mass inside control volume at time t
m(t +dt) = total mass inside at time (t + dt)
e(t) = u + V2/2 + gz = specific energy of matter inside the
control volume at time t
e(t + dt) = specific energy of matter at time (t + dt)
Piand Pe= pressure at inlet and exit ports
Viand Ve= velocity at inlet and exit ports
viand ve= specific volume at inlet and exit ports
eiand ee= specific energy at inlet and exit ports
Writingmassbalance,
Workdonebysurroundingoncontrolvolume,bycompressing
massAincontrolvolume=
Workdoneonsurroundingoncontrolvolume,releasingmass
Bfromcontrolvolume=
Energyofsystemattimet=
Energyofsystemattime(t+dt)=
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Applyingfirstlawofthermodynamicsfortimeintervaldt,
E2 E1=Q W
Rearranginganddividebydt,
Uselimitdt0 ute=u+V2/2+ z andh=u+Pv
Rearranging,
Inwords,
Rateofenergyaccumulation=Rateofenergyinflow
Rateofenergyoutflow
Note:Aboveequationisusefulforanalysisofunsteadyflow
processes.
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SteadyStateFlowProcess In any steady state flow process,
= constant
and dm/dt = 0, m = constant (no accumulation)
The state of matter at the inlet, exit and at any given point
inside control volume does not change with time.
Therefore, dE/dt = 0, E = constant,
,
First law for steady state open system (SFE),
ApplicationsofsteadystateflowprocessesTurbine
High pressure steam, expanded to a lower pressure with help
of nozzles
Pressure energy converted into kinetic energy
High velocity fluid impacts on set of blades
Delivering of shaft work
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Writing first law for steady flow process,
Ignoring heat losses, small change in kinetic and potential
energy through a turbine,
Compressor
Operatinginreverseofturbine
,
Ignoringheatlosses,kineticandpotentialenergychange,
Here,he>hi
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Nozzle
Primarilyusedtoincreaseflowvelocity
,
Neglectingpotentialenergyforanadiabaticnozzle,
Ifinletvelocityisnegligible(Vi0),
Ve={2(hi he)}
Foridealgas,puthi he=CP(Ti Te)above,
V ={2C (T T )}
Ve={2CPTi(1 Te/Ti)}
Particularlyforadiabaticexpansionthroughnozzle,
PutthisinVeabove,
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Diffuser
Canbethoughtasreversetonozzle
Firstlawanalysisforanadiabaticdiffuser,
HeatExchanger/Condenser
Transferofenergyasheatfromonefluidtoanother
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First law for a heat exchanger can be written as,
As, shaft work = 0, heat losses = 0 and change in
kinetic and potential energy = small
Therefore,
ThrottlingValves
Flowrestricting devices that cause a significant
pressure drop in the fluid Pressure drop in the fluid is often accompanied by a
large drop in temperature (or, sometimes, the
temperature rise)
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Small devices, flow may be assumed to be adiabatic(Q = 0), since neither sufficient time nor largeenough area for any effective heat transfer to take
place
Writing first law for steady state device,
No shaft work (Wsh = 0), small potential energychange and insignificant increase in kinetic energy,So
hi= he (Isenthalpic device)
or ui+ Pivi= ue+ Peve
MixingChambersWritingfirstlawforsteadyflow,
Ignoringheattransfer,shaftwork,potentialandkinetic
energychanges,
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TransientFlowProcesses Unsteadyflowprocesses
Differentmassflowrates(inandout)
Propertiesincontrolvolumevarywithtime
Charginganddischargingofagascylinder
Chargingofacylinder
Considercylinderascontrolvolumeandwritingfirst
lawforunsteadyflowsystems,
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Here,
Ignoringchangeinpotentialandkineticenergy
Equationreducesto,
Where,m=massofgasincontrolvolumeattimet
and u = s ecific internal ener in control volume at
timet.
Integrateaboveeq.fromstartofchargingoperation
(t=0)toendofchargingoperation(t=t),
Writingmassbalanceforcontrolvolume,
Integratingfromtimet=0totimet,
Putvalueinequation(1),
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Dischargingofacylinder
Writing first law for flow process across control
volume
Here,
Ignoringpotentialenergychange
Integratingfromtimet=0totimet,
Writingmassbalancefordischarging,
Integrating,
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Putthisvalueinequation(2),
Example(Dischargingofacylinder):A 750 L rigid tank, shown in figure 3, initially contains water at250C and 50% liquid and 50% vapour by volume. A valve at the
bottom of the tank is opened and liquid is slowly withdrawn.
Heat transfer takes place such that the temperature remains
cons an . n e amoun o ea rans er requ re o e s a e
where half the initial mass is withdrawn.
Solution:
Writing equation for discharging a cylinder with neglecting
,
Usesat.temperaturetableat250C,
vf=0.001251m3/kg,vg=0.0500037m
3/kg
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So,massofliquid=mf=0.375/0.001251=299.76kg
andmassofvapour =mg=0.375/0.050037=7.49kg
Totalinitialinternalenergyintankm0u0=mfuf+mgug=mf(hf Psatvf)+mg(hg Psatvg)
= 299.76 1085.8 3977.6*0.001251 + 7.49 2800.43977.6*0.050037)=343464kJ
Initialtotalmass=299.76+7.49=307.25kg
Finalmassintank=(307.25)/2=153.63kg
Infinalstate(250C),specificvolumevf=0.75/153.63
=0.004882m3/kg
Atfinalstate,usev=x.vg+(1 x)vf0.004882=xfinal(0.050037)+(1 xfinal)0.001251
xf=0.074
Now,ufinal =xfinal.ug+(1 xfinal)uf
=xfinal(hg Psatvg)+(1 xfinal)(hf Psatvf)=0.074(2800.4 3977.6*0.050037)+(1 0.074)(1085.8
3977.6*0.001251)
=193.45kJ/kg (bysteamtable)
=1151.87
Also,he=hf=enthalpyofliquidwithdrawing
=1085.34kJ/kg
Puttingallvalueinenergyequationabove,Q=6450kJ