1st law control vol

Upload: raghav-bahadur-saxena

Post on 06-Apr-2018

228 views

Category:

Documents


0 download

TRANSCRIPT

  • 8/3/2019 1st Law Control Vol

    1/10

    9/7/20

    1

    First Law Analysis for aControl Volume (open system)

    Control Volume A control volume is a volume in space in which

    we have interest for a particular study oranalysis. The surface of this control volume is

    called the control surface. The size and shape of control volume are

    arbitrarily chosen to suit our analysis.

    The surface may be fixed, or it may be movable(expand or contract).

    Mass as well as heat and work can cross thecontrol surface, and the mass in the control

    volume (as well as its properties) change withtime.

    2

    Control Volume

    3

    Mass Balance When we have many flows coming in and

    going out of the control volume,

    4

    massin massout

    controlvolume

    ei

    C.V. mmdt

    dm

    So, if the mass inside thecontrol volume changes withtime, it is only because we addsome mass or take out some

    mass. There can be NO othermeans by which mass inside a

    control volume can change.

    The above equation iscalled Conservation of

    Mass or Continuity

    Equation.

    The first law of thermodynamics fora control volume

    The first law for a control mass,1Q2 1W2 = E = E2 E1

    The rate form of first law for control mass,

    5

    WQdt

    dE MC ..

    In a similar manner, a control volume willhave rates of heat transfer, rates of work, and(in addition) mass flows.

    Mass and Volume Flow Rates

    The amount of mass flowing through a cross-section per unit time is called the mass flow

    rate. A liquid or gas flows in and out of a control

    volume through pipes or ducts. The mass flowrate of a fluid flowing in a pipe is proportionalto the cross-sectional area A of the pipe, thedensity of the fluid, and the velocity of thefluid.

    The mass flow rate through a differential areadA is given by,

    6

    dAVmd nWhere nV is the velocity component normal to dA.

  • 8/3/2019 1st Law Control Vol

    2/10

    9/7/20

    Mass and Volume Flow Rates

    The mass flow rate through the entire cross-

    sectional area of the pipe is obtained byintegration:

    7

    dAVmdn

    dAVm n

    In most practical applications, the flow of fluidthrough a pipe can be approximated to be one-dimensional flow. This means, properties can beassumed to vary in one direction only (the directionof flow). So, the properties are uniform at any cross-section normal to the flow direction.

    Mass and Volume Flow Rates

    Here, is density (=1/v), kg/m3 , A is cross-

    sectional area normal to flow direction, m2

    .The volume of the fluid flowing through a cross-

    section per unit time is called the volume flowrate, given by,

    8

    vVAAVdAVm n /

    AVdAVVA

    n

    The mass and volume

    flow rates are related

    by

    )(velAv

    VVm

    The concept of Flow EnergyFor control volumes, an additional mechanism

    can change the energy of a system: mass flowin and out of the control volume.

    When mass enters a control volume, the energy ofa control volume increases because the enteringmass carries some energy with it.

    Similarly, when some mass leaves the controlvolume, the energy contained within the control

    volume decreases because the leaving masstakes out some energy with it.

    9

    Total Energy of a flowing fluid

    10

    gzV

    upekeue2

    2

    The fluidpossesses anadditional formof energy __the flow energy(flow work).

    The fluid flowing across the control surfaceenters or leaves with an amount of energy perunit mass as,

    whenever a fluid mass enters a control volume atstate i, or exits at state e, there is a boundarymovement work associated with that process.

    Flow WorkControl volumes involve flow of mass across the

    control surfaces, and some work is required to

    push the mass into or out of the control volume.This work is known as the flow work. It is

    necessary for maintaining a continuous flowthrough the control volume.

    Consider a fluid element of volume V just enteringthe control volume. The fluid immediatelyupstream will force this fluid element to enterthe control volume; thus it can be regarded as an

    imaginary piston.11

    Flow Work..

    If the fluid pressure is P and the cross-sectionalarea of the element is A, the force applied on

    the fluid element by the imaginary piston is:F = P A

    To push the entire fluid element into the controlvolume, this force acts through a distance X;thus the work done in pushing the fluidelement across the boundary (flow work) is:

    WFLOW = P A X = P V

    So, the flow work per unit mass is given by,

    wFLOW = P v

    12

  • 8/3/2019 1st Law Control Vol

    3/10

    9/7/20

    Flow work.

    The rate of flow work is,

    13

    mPvVPdAVPVFdtdxFW flow /.

    For the flow that leaves the control volume,work is being done by the control volume,

    eeemvP

    and for the mass that enters, the surroundingsdo the rate of work equal to

    iii mvP

    Flow work

    The flow work per unit mass is then Pv, and thetotal energy associated with the flow of mass is,

    14

    The first law equation control volume case,

    gz2

    2Vhgz

    2

    2VPvuPve

    )eedtdE

    e.V .C.V.C.V.

    )z2V( hz2

    V( hdtdE

    e2

    ee2ii.V .C.V.C.V.

    Flow work

    15

    Here, the work term W accounts for all other typesof work (shaft work, boundary work, etc.) exceptflow work.For a general control volume where we may havemultiple mass streams entering the control

    volume, and multiple mass streams leaving the

    control volume-

    )z2V( hz2

    V( hdtdE

    e2

    ee2ii.V .C.V.C.V.

    )z2V( hz2

    V( hdtdE

    e2

    ee2ii.V .C.V.C.V.

    )z2V( hz2

    V( hdtdE

    e2

    ee2ii.V .C.V.C.V.

    This means that :--------The rate of change of energy inside the control

    volume is due to :--A net rate of heat transfer,A net rate of work andThe summation of energy fluxes due to mass

    flows into and out of a control volume.

    16

    First Law for a control volume

    Note that:

    is the net rate of energy changewithin the CV (it is zer o for st eady-state, steady flow systems)

    are terms representing fluxes ofenergy into and out of the CV,

    which depend on the massfluxes.

    are terms representing energytransfer across the CV boundariesnot associated with the massfluxes.

    17

    dtdEcv

    2V

    m(h gz)2

    cv cvQ and W :

    The steady stateprocess

    18

  • 8/3/2019 1st Law Control Vol

    4/10

    9/7/20

    When is a system at equilibrium?

    For a system to be at equilibrium there can beno processes occurring within the system.

    19

    i.e. It must be at the same temperature as thatof surroundings.

    Steady state is not the same asequilibrium

    Equilibrium

    20

    0xT 0

    tT

    At equilibrium the temperature is thesame throughout the system, and itdoes not change with time.

    Steady State

    21

    0x

    T0

    t

    T

    At steady state different temperaturescan exist at different points around the

    system, but the system does notchange with time.

    22

    First Law Analysisfor a Control

    Volume

    Contd

    Open Systems: Steady State Steady Flow

    (SSSF)

    Steady-state (SS): The state of a substancewithin Control Volume does not change withrespect to time.

    Steady-flow (SF): the total mass within aControl Volume does not change with respectto time.

    WE deal with steady-state, steady-flow (SSSF)system now onwards

    23

    Assumptions of the steady statemodel

    No change in the mass of fluid in theCV i.e. Mass in = Mass out.

    Fluid is uniform in state and incomposition.

    State of fluid at any point is same at alltime.

    Heat and work interaction betweensystem & surroundings across controlsurface dont change with time.

    24

  • 8/3/2019 1st Law Control Vol

    5/10

    9/7/20

    Assumption: The state of mass at each point in thecontrolvolumedoes notvarywithtime.

    Consequence:

    25

    0..

    dt

    dmVC 0..

    dt

    dE VC

    So, for the steady state process:Continuity equation:

    eimm

    ..

    22

    .. )2

    ()2

    ( VCee

    eeii

    iiVC WgzV

    hmgzV

    hmQ

    First Law becomes for steady state process,

    )2

    ()2

    (

    22

    ....

    ..

    ee

    eeii

    iiVCVCVC gz

    Vhmgz

    VhmWQ

    dt

    dE

    When we have only one stream entering thecontrol volume and only one stream leaving,

    Continuity equation:

    26

    mmmei

    ..

    22

    .. )2

    ()2

    ( VCee

    eeii

    iiVC WgzV

    hmgzV

    hmQ

    First Law

    m

    Qq VC ..Define and

    m

    Ww VC ..

    wgzV

    hgzV

    hq ee

    eii

    i22

    22

    27

    STEADY- FLOWENGINEERING

    DEVICES

    Some common steady flow devices

    28

    Only one input & one output

    Single Stream Steady FlowSystem

    Nozzles

    Diffusers

    Turbines

    Compressors

    Throttling Valve

    29

    ieie

    ie zzgVV

    hhmWQ2

    22

    Nozzles and Diffusers arecommonly used in jetengines, rockets,spacecrafts and even ingarden hoses.

    30

    Nozzles and Diffusers

  • 8/3/2019 1st Law Control Vol

    6/10

    9/7/20

    Nozzles

    A nozzle is a steady

    state device thatincreases thevelocity of a fluidat the exit/ outletpoint at expenseof pressure.

    31

    Nozzles

    32

    There is no means to doany work in a nozzle,

    since there are no movingparts.The kinetic energy of thefluid at the nozzle inlet isusually small, and would

    be neglected if its value isnot known.

    Diffuser A steady state diffuser is a device constructed

    to slow down a high-velocity fluid in a manner

    that results in an increase in the pressure ofthe fluid at the exit.

    In a way, it is an EXACT OPPOSITE of a

    nozzle.

    There is large kinetic energy at the diffuser

    inlet and a small, (but usually not negligible)kinetic energy at the exit.

    33

    NOZZLES & DIFFUSERS. These are assumed to be adiabatic devices

    because flow thru these devices are at highvelocities, so there is NO significant change inheat transfer.

    Also there is NO work interactions, since theyare used for acceleration & deceleration of flowonly.

    Also there is no change in elevation of flowthrough these devices.

    34

    Nozzles and Diffusers

    35

    ieie

    ie zzgVV

    hhmWQ2

    22

    Is there work interaction in this system? NO

    Is there heat transfer?

    Does the fluid change elevation? NO

    20

    22

    ieie

    VVhh

    NO

    20

    22

    ieie

    VVhh

    How can you find the mass flow rate

    in a nozzle?e

    ee

    i

    ii

    v

    AV

    v

    AVm

    In a nozzle, enthalpy is converted

    into kinetic energy

    36

    )h2(hVe eiIf inlet velocity is neglected,then exit velocity is given by

  • 8/3/2019 1st Law Control Vol

    7/10

    9/7/20

    Throttling Valves

    A throttling process occurswhen a fluid flowing in aline suddenly encounters

    a restriction in the flowpassage.

    This may be a plate with asmall hole in it, a partiallyclosed valve protrudinginto the flow passage, or itmay be a change to amuch smaller diametertube, such as capillary.

    37

    Throttling ValveThe result of this

    restriction is an abruptpressure drop in thefluid, as it is forced to

    find its way through asuddenly smallerpassage way.

    A steady state throttlingprocess isapproximately apressure drop atconstant enthalpy.

    38

    Throttling Valve

    Throttling valves are adiabatic because

    there is neither sufficient time & nor largearea for any effective heat transfer to take

    place.

    Also NO work interaction takes place in

    these Valves.

    Change in fluid elevation is also ignored.

    Usually change in K.E of fluid is alsoneglected.

    39

    ieie

    ie zzgVV

    hhmWQ2

    22

    Throttling Valve

    40

    Is there work in this system? NO

    Is there heat transfer? NO

    Does the fluid change elevation? NO

    Does the fluid change velocity? Usually it can be ignored

    iehh0

    Throttling Valves

    hin = hout

    For ideal gasesh = Cp T

    But h = 0

    So T = 0

    The inlet and outlet temperatures are the same!!!

    Throttling Valves are sometimes called asisenthaplic devices.

    41

    Turbine

    A turbine is a rotary

    steady state machine whose purpose is toproduce shaft work(power) at theexpense of the

    pressure of theworking fluid.

    42

  • 8/3/2019 1st Law Control Vol

    8/10

    9/7/20

    Turbine

    Inside the turbine, there are two distinctprocesses:

    In the first, the working fluid passes through a

    set of nozzles, that expand the fluid to a lowerpressure and higher velocity.

    In the second, this high-velocity fluid stream isdirected onto a set of moving (rotating) blades,in which the velocity is reduced before beingdischarged from the outlet. This produces atorque on the rotating shaft, resulting in a shaftwork output.

    43

    The purpose of a steady statecompressor (gas) or pump (liquid) is:

    To increase the pressure of a fluid byputting in shaft work (power).

    The working fluid enters thecompressor at low pressure, movinginto a set of rotation blades, fromwhich it exits at higher velocity, as aresult of the shaft work on the fluid.The fluid then passes through adiffuser section, in which it is sloweddown in a way that increases itspressure. So, fluid finally exits fromthe compressor at high pressure.

    44

    Compressors

    Turbines and Compressors

    45

    A turbine is a device thatproduces work at the expense oftemperature and pressure.

    A compressor is a device thatincreases the pressure of a fluid by

    adding work to the system.

    ieie

    ie zzgVV

    hhmWQ2

    22

    Turbines and Compressors

    46

    Is there work in this system? Yes!

    Is there heat transfer? Usually it can be ignored

    Does the fluid change elevation? Usually it can be ignored

    Does the kinetic energy change? Usually it can be ignored

    iehhmW iehhw

    Mixing of Streams

    47

    Mixing Chamber

    48

    Mixing two or more fluids

    is a common engineeringprocess.

    Mixing

    Chamber

  • 8/3/2019 1st Law Control Vol

    9/10

    9/7/20

    Mixing Chamber

    49

    i

    i

    iie

    e

    eegz

    Vhmgz

    Vhm

    netnet WQ 22

    22

    We no longer have only one inlet and one exit stream

    Is there any work done? No

    Is there any heat transferred? No

    Is there a velocity change? No

    Is there an elevation change? Usually it can be ignored

    iiee hmhm0

    Mixing Chamber

    Mass Balance

    50

    iemm

    51

    Mixing Chamber

    52

    332211 hmhmhm

    321 mmm

    Energy

    Balance

    Mass

    Balance

    Heat Exchanger

    53

    Heat Exchanger

    54

    A heat exchanger is adevice where twomoving fluids exchangeheat without mixing.

  • 8/3/2019 1st Law Control Vol

    10/10

    9/7/20

    Heat Exchangers

    55

    Our analysis approach will depend on howwe define your system