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