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MASS & ENERGY
ANALYSIS OF CONTROL
     SYSTEMS
                                  Lecture 8

         Keith Vaugh BEng (AERO) MEng



 Reference text: Chapter 6 - Fundamentals of Thermal-Fluid Sciences, 3rd Edition
                    Yunus A. Cengel, Robert H. Turner, John M. Cimbala
                                    McGraw-Hill, 2008
                                                                                   KEITH VAUGH
OBJECTIVES
             }

             KEITH VAUGH
OBJECTIVES
Develop the conservation of mass principle.
                                              }

                                              KEITH VAUGH
OBJECTIVES
Develop the conservation of mass principle.

Apply the conservation of mass principle to various
systems including steady- and unsteady-flow control
                                                      }
volumes.




                                                      KEITH VAUGH
OBJECTIVES
Develop the conservation of mass principle.

Apply the conservation of mass principle to various
systems including steady- and unsteady-flow control
                                                           }
volumes.

Apply the first law of thermodynamics as the statement of
the conservation of energy principle to control volumes.




                                                           KEITH VAUGH
OBJECTIVES
Develop the conservation of mass principle.

Apply the conservation of mass principle to various
systems including steady- and unsteady-flow control
                                                            }
volumes.

Apply the first law of thermodynamics as the statement of
the conservation of energy principle to control volumes.

Identify the energy carried by a fluid stream crossing a
control surface as the sum of internal energy, flow work,
kinetic energy, and potential energy of the fluid and to
relate the combination of the internal energy and the flow
work to the property enthalpy.

                                                            KEITH VAUGH
}

KEITH VAUGH
Solve energy balance problems for common steady-flow
devices such as nozzles, compressors, turbines, throttling
valves, mixers, heaters, and heat exchangers.
                                                             }

                                                             KEITH VAUGH
Solve energy balance problems for common steady-flow
devices such as nozzles, compressors, turbines, throttling
valves, mixers, heaters, and heat exchangers.
                                                             }
Apply the energy balance to general unsteady-flow
processes with particular emphasis on the uniform-flow
process as the model for commonly encountered charging
and discharging processes.




                                                             KEITH VAUGH
CONSERVATION OF MASS
   Conservation of mass
                                                           }
   Mass, like energy, is a conserved property, and it cannot
   be created or destroyed during a process.

   Closed systems
   The mass of the system remain constant during a
   process.

   Control volumes
   Mass can cross the boundaries, and so we must keep
   track of the amount of mass entering and leaving the
   control volume.




                                                           KEITH VAUGH
Mass is conserved
even during chemical
reactions




                KEITH VAUGH
Mass is conserved
                                                        even during chemical
                                                        reactions




Mass m and energy E can be converted to each other according to

     E = mc 2

where c is the speed of light in a vacuum, which is c = 2.9979 × 108 m/s.
The mass change due to energy change is absolutely negligible.



                                                                        KEITH VAUGH
MASS & VOLUME FLOW RATES
  &
δ m = ρVn dAc
  &       &
  m = ∫ δ m = ∫ ρVn dAc
         Ac                Ac
                                                                                          }
         1                      Definition of
Vavg   =      ∫        Vn dAc
         Ac       Ac            average velocity
                                                   The average velocity Vavg is defined as the
                                                   average speed through a cross section.




                                                                                       KEITH VAUGH
MASS & VOLUME FLOW RATES
  &
δ m = ρVn dAc
  &       &
  m = ∫ δ m = ∫ ρVn dAc
         Ac                Ac
                                                                                          }
         1                      Definition of
Vavg   =      ∫        Vn dAc
         Ac       Ac            average velocity
                                                   The average velocity Vavg is defined as the
                                                   average speed through a cross section.

  &
  m = ρVavg Ac                  ( s)
                                kg




                                                                                       KEITH VAUGH
MASS & VOLUME FLOW RATES
  &
δ m = ρVn dAc
  &       &
  m = ∫ δ m = ∫ ρVn dAc
         Ac                Ac
                                                                                            }
         1                        Definition of
Vavg   =      ∫        Vn dAc
         Ac       Ac              average velocity
                                                     The average velocity Vavg is defined as the
                                                     average speed through a cross section.

  &
  m = ρVavg Ac                    ( s)
                                   kg

           &
           V
  &    &
  m = ρV =                      Mass flow rate
           v




                                                                                         KEITH VAUGH
MASS & VOLUME FLOW RATES
  &
δ m = ρVn dAc
  &       &
  m = ∫ δ m = ∫ ρVn dAc
         Ac                Ac
                                                                                              }
         1                        Definition of
Vavg   =      ∫        Vn dAc
         Ac       Ac              average velocity
                                                       The average velocity Vavg is defined as the
                                                       average speed through a cross section.

  &
  m = ρVavg Ac                    ( s)
                                   kg

           &
           V
  &    &
  m = ρV =                      Mass flow rate
           v
  Volume flow rate

  &
  V = ∫ Vn dAc = Vavg Ac = VAc
         Ac                                     ( s)
                                                m3

                                                                                           KEITH VAUGH
MASS & VOLUME FLOW RATES
  &
δ m = ρVn dAc
  &       &
  m = ∫ δ m = ∫ ρVn dAc
         Ac                Ac
                                                                                              }
         1                        Definition of
Vavg   =      ∫        Vn dAc
         Ac       Ac              average velocity
                                                       The average velocity Vavg is defined as the
                                                       average speed through a cross section.

  &
  m = ρVavg Ac                    ( s)
                                   kg

           &
           V
  &    &
  m = ρV =                      Mass flow rate
           v
  Volume flow rate

  &
  V = ∫ Vn dAc = Vavg Ac = VAc
         Ac                                     ( s)
                                                m3       The volume flow rate is the
                                                         volume of fluid flowing through
                                                         a cross section per unit time.
                                                                                           KEITH VAUGH
CONSERVATION OF MASS
                    PRINCIPLE

    The conservation of mass principle for a control volume
    The net mass transfer to or from a control volume during a time
    interval Δt is equal to the net change (increase or decrease) in
                                                                         }
    the total mass within the control volume during Δt.



⎛ Total mass entering ⎞ ⎛ Total mass leaving ⎞ ⎛ Net change in mass ⎞
⎜ the CV during Δt ⎟ − ⎜ the CV during Δt ⎟ = ⎜ within the CV during Δt ⎟
⎝                     ⎠ ⎝                    ⎠ ⎝                        ⎠




                                                                        KEITH VAUGH
min − mout = Δmcv   ( kg )
                                                              dmcv
                                                 & &
                                                 min − mout =
                                                               dt    ( s)
                                                                      kg




Conservation of mass principle for an ordinary
bathtub



                                                                         KEITH VAUGH
min − mout = Δmcv               ( kg )
                                                              dmcv
                                                 & &
                                                 min − mout =
                                                               dt                ( s)
                                                                                  kg


                                                 General conservation of mass

                                                 d                       r r
                                                 dt   ∫
                                                      cv
                                                           ρ dV + ∫
                                                                  cs
                                                                        (    )
                                                                       ρ V ⋅ n dA = 0




Conservation of mass principle for an ordinary
bathtub



                                                                                     KEITH VAUGH
min − mout = Δmcv                    ( kg )
                                                              dmcv
                                                 & &
                                                 min − mout =
                                                               dt                     ( s)
                                                                                       kg


                                                 General conservation of mass

                                                 d                       r r
                                                 dt   ∫
                                                      cv
                                                           ρ dV + ∫
                                                                  cs
                                                                        (         )
                                                                       ρ V ⋅ n dA = 0


                                                 General conservation of mass
                                                 in rate form

                                                 d
                                                      ∫             &     &
                                                           ρ dV = ∑ m − ∑ m
                                                 dt   cv
                                                                  in        out
Conservation of mass principle for an ordinary
bathtub                                             dmcv
                                                 or           &
                                                         = ∑m − ∑m  &
                                                     dt    in   out

                                                                                          KEITH VAUGH
MASS BALANCE FOR STEADY
        FLOW PROCESSES
 During a steady-flow process, the total amount of mass
 contained within a control volume does not change with time
 (mCV = constant).
                                                                    }
 Then the conservation of mass principle requires that the total
 amount of mass entering a control volume equal the total
 amount of mass leaving it.




                                                                   KEITH VAUGH
For steady-flow processes, we are
interested in the amount of mass
flowing per unit time, that is, the mass
flow rate

 &
in
      &
∑m = ∑m
       out
                  ( s)
                   kg       Multiple inlets
                            and exits


& &
m1 = m2 → ρV1 A1 = ρV2 A2       Single
                                stream


Many engineering devices such as
nozzles, diffusers, turbines,
compressors, and pumps involve a
single stream (only one inlet and one         Conservation of mass principle for a two
outlet).                                      inlet - one outlet steady flow system




                                                                                KEITH VAUGH
Special case: Incompressible Flow
The conservation of mass relations can be simplified even further when the
fluid is incompressible, which is usually the case for liquids.

                                &    &
                               ∑V = ∑V
                               in     out
                                                   ( s)
                                                    m3

                               & &
                               V1 = V2 → V1 A1 = V2 A2

                               There is no such thing as a “conservation of
                               volume” principle.

                               However, for steady flow of liquids, the volume
                               flow rates, as well as the mass flow rates, remain
                               constant since liquids are essentially
During a steady-flow process,   incompressible substances.
volume flow rates are not
necessarily conserved
although mass flow rates are.                                            KEITH VAUGH
FLOW WORK & THE ENERGY
     OF A FLOWING FLUID
Flow work, or flow energy
The work (or energy) required to push the mass into or out of the
control volume. This work is necessary for maintaining a
continuous flow through a control volume.
                                                                                           }

In the absence of acceleration, the force applied on a fluid by a piston is equal to the force applied
on the piston by the fluid.
                                                                                              KEITH VAUGH
FLOW WORK & THE ENERGY
     OF A FLOWING FLUID
Flow work, or flow energy
The work (or energy) required to push the mass into or out of the
control volume. This work is necessary for maintaining a
continuous flow through a control volume.
                                                                                           }

In the absence of acceleration, the force applied on a fluid by a piston is equal to the force applied
on the piston by the fluid.
                                                                                              KEITH VAUGH
F = PA
                         W flow = FL = PAL = PV   ( kJ )

                         W flow = Pv    ( kg)
                                         kJ



Schematic for flow work




                                                  KEITH VAUGH
TOTAL ENERGY OF A
                    FLOWING FLUID

e = u + ke + pe = u +
                      V2
                      2
                         + gz      ( kg)
                                   kJ
                                           }
θ = Pv + e = Pv + ( u + ke + pe)




                                           KEITH VAUGH
TOTAL ENERGY OF A
                    FLOWING FLUID

e = u + ke + pe = u +
                      V2
                      2
                         + gz      ( kg)
                                   kJ
                                                               }
θ = Pv + e = Pv + ( u + ke + pe)

But the combination Pv + u has been previously defined as the
enthalpy h




                                                               KEITH VAUGH
TOTAL ENERGY OF A
                    FLOWING FLUID

e = u + ke + pe = u +
                      V2
                      2
                         + gz      ( kg)
                                    kJ
                                                                     }
θ = Pv + e = Pv + ( u + ke + pe)

But the combination Pv + u has been previously defined as the
enthalpy h
                                           The flow energy is automatically
                      V2
θ = h + ke + pe = h +
                      2
                         + gz      ( kg)
                                   kJ      taken care of by enthalpy. In
                                           fact, this is the main reason for
                                           defining the property enthalpy.




                                                                        KEITH VAUGH
The total energy consists of three parts for a non-flowing fluid and four parts for a
flowing fluid.




                                                                                      KEITH VAUGH
ENERGY TRANSPORT BY
                    MASS
Amount of energy transport

        Emass
                         ⎛
                = mθ = m ⎜ h +
                         ⎝
                                V2
                                2
                                        ⎞
                                   + gz ⎟
                                        ⎠
                                                       ( kJ )
                                                                }
Rate of energy transport

       &                 ⎛     V2      ⎞
       Emass      &    &
                = mθ = m ⎜ h +    + gz ⎟             ( kW )
                         ⎝     2       ⎠




                      The product ṁiθi is the energy
                  transported into control volume by
                                  mass per unit time
                                                                KEITH VAUGH
When the kinetic and potential
                                     energies of a fluid stream are
                                     negligible

                                       Emass = mh
                                       &       &
                                       Emass = mh

The product ṁiθi is the energy       When the properties of the mass at
transported into control volume by   each inlet or exit change with time
mass per unit time.
                                     as well as over the cross section

                                                                     ⎛    Vi 2       ⎞
                                       Ein,mass   = ∫ θ i δ mi = ∫ ⎜ hi +      + gzi ⎟ δ mi
                                                     mi           mi ⎝     2         ⎠



                                                                                   KEITH VAUGH
ENERGY TRANSPORT BY
              MASS
         Many engineering systems
         such as power plants operate
         under steady conditions.
                                        }

                                        KEITH VAUGH
Under steady-flow conditions, the mass     Under steady-flow conditions, the fluid
and energy contents of a control volume      properties at an inlet or exit remain
remain constant.                             constant (do not change with time).




                                                                         KEITH VAUGH
Mass and energy balances for a steady-flow process

       &    &
      ∑m = ∑m
       in     out

         & &
        m1 = m2         Mass
    ρ1V1 A1 = ρ2V2 A2   balance




                                                A water heater in steady operation.




                                                                         KEITH VAUGH
Mass and energy balances for a steady-flow process

         &    &
        ∑m = ∑m
          in          out

          & &
         m1 = m2                           Mass
     ρ1V1 A1 = ρ2V2 A2                     balance


Energy balances
                                                           Z   0
                                             dEsystem
        & &
        Ein − Eout               =                                         =0
        14 2 4 3                               dt 3
   Rate of net energy transfer               14 2 4
    by heat, work and mass              Rate of change in internal,
                                     kinetic, potential, etc... energies
                                                                                A water heater in steady operation.




                                                                                                         KEITH VAUGH
Mass and energy balances for a steady-flow process

            &    &
           ∑m = ∑m
            in           out

             & &
            m1 = m2                           Mass
        ρ1V1 A1 = ρ2V2 A2                     balance


Energy balances
                                                              Z   0
                                                dEsystem
           & &
           Ein − Eout               =                                         =0
           14 2 4 3                               dt 3
     Rate of net energy transfer                14 2 4
      by heat, work and mass               Rate of change in internal,
                                        kinetic, potential, etc... energies
                                                                                   A water heater in steady operation.
            &
            Ein                =            &
                                            Eout                         ( kW )
            {                               {
 Rate of net energy transfer       Rate of net energy out,
  by heat, work and mass           by heat, work and mass




                                                                                                            KEITH VAUGH
Mass and energy balances for a steady-flow process

            &    &
           ∑m = ∑m
            in           out

             & &
            m1 = m2                           Mass
        ρ1V1 A1 = ρ2V2 A2                     balance


Energy balances
                                                              Z   0
                                                dEsystem
           & &
           Ein − Eout               =                                         =0
           14 2 4 3                               dt 3
     Rate of net energy transfer                14 2 4
      by heat, work and mass               Rate of change in internal,
                                        kinetic, potential, etc... energies
                                                                                   A water heater in steady operation.
            &
            Ein                =            &
                                            Eout                         ( kW )
            {                               {
 Rate of net energy transfer       Rate of net energy out,
  by heat, work and mass           by heat, work and mass


                         ⎛
           & + Win + ∑ m h +
                &            V2      ⎞ &                  ⎛
                                                  & + ∑m h +  V2      ⎞
           Qin          &⎜     + gz ⎟ = Qout + Wout     &⎜    + gz ⎟
                         ⎝   2      ⎠                    ⎝  2      ⎠
                     1 4 44 2 4 4 4
                     in
                                   3                  1 4 44 2 4 4 4
                                                      out
                                                                    3
                                            for each inlet                              for each exit

                                                                                                            KEITH VAUGH
Energy balance relations with sign conventions (i.e., heat input and work
output are positive)

                    ⎛
      &− W = + ∑ m h +
          &            V2      ⎞       ⎛     V2      ⎞
      Q            &⎜                &
                          + gz ⎟ − ∑ m ⎜ h +    + gz ⎟
                    ⎝  2      ⎠ in ⎝        2       ⎠
               1 4 44 2 4 4 4
               out
                             3 1 4 44 2 4 4 4        3
                          for each exit               for each inlet


               ⎡
       &− W = m h2 − h1 +
           & &            V22 − V12                 ⎤
       Q       ⎢                   + g ( z2 − z1 ) ⎥
               ⎣             2                     ⎦

                          V22 − V12
        q − w = h2 − h1 +           + g ( z2 − z1 )
                              2

        q − w = h2 − h1
            Q&
        q=
            W&
            W&
        w=
             &
             m
                                               Refer to pages, 212 - 214   KEITH VAUGH
STEADY FLOW
    ENGINEERING DEVICES
Many engineering devices operate essentially under the same
conditions for long periods of time. The components of a steam
power plant (turbines, compressors, heat exchangers, and
                                                                  }
pumps), for example, operate nonstop for months before the
system is shut down for maintenance. Therefore, these devices
can be conveniently analysed as steady-flow devices.



                                            A modern land-based gas turbine
                                            used for electric power
                                            production. This is a General
                                            Electric LM5000 turbine. It has a
                                            length of 6.2 m, it weighs 12.5
                                            tons, and produces 55.2 MW at
                                            3600 rpm with steam injection.

                                                                    KEITH VAUGH
Nozzles and Diffusers
Commonly utilised in jet engines, rockets,
spacecraft, and even garden hoses.

A nozzle is a device that increases the
velocity of a fluid at the expense of pressure.

A diffuser is a device that increases the
pressure of a fluid by slowing it down.

The cross-sectional area of a nozzle decreases
in the flow direction for subsonic flows and
increases for supersonic flows. The reverse is
                                                         Nozzles and diffusers are shaped so
true for diffusers.
                                                         that they cause large changes in fluid
                                                         velocities and thus kinetic energies.
              & &
              Ein = Eout

      ⎛     V12 ⎞  ⎛     V22 ⎞                &       &
    &               &
    m ⎜ h1 + ⎟ = m ⎜ h2 + ⎟        Since      Q ≅ 0, W ≅ 0, and      Δpe ≅ 0
      ⎝      2 ⎠   ⎝      2 ⎠
                                            Refer to Example 6-4 & 6-5, page 216/7   KEITH VAUGH
Turbines and compressors
Turbine drives the electric generator in power
plants. As the fluid passes through the turbine,
work is done against the blades, which are
attached to the shaft. The shaft rotates, and the
turbine produces work.

Compressors, as well as pumps and fans,
increase the pressure of a fluid. Work is
supplied to these devices from an external
source through a rotating shaft.                    Energy balance for the compressor
                                                    in this figure:
A fan increases the pressure of a gas slightly
and is mainly used to mobilise a gas.                        & &
                                                             Ein = Eout
                                                      & &        &      &
                                                     Win + mh1 = Qout + mh2
A compressor is capable of compressing the gas
to very high pressures.                              Since
                                                     Δke = Δpe ≅ 0
Pumps work very much like compressors
                                                    Refer to Example 6-6 & 6-7, page 218/9
except that they handle liquids instead of gases.                             KEITH VAUGH
Throttling valves
Throttling valves are any kind of flow-
restricting devices that cause a significant
pressure drop in the fluid.

The pressure drop in the fluid is often
accompanied by a large drop in
temperature and for that reason throttling    The temperature of an ideal gas does not
                                              change during a throttling (h = constant)
devices are commonly used in refrigeration
                                              process since h = h(T).
and air-conditioning applications.

      h2 ≅ h1                     Energy
                                  balance
      u1 + P1v1 = u2 + P2 v2

Internal energy + Flow Energy = Constant

 Refer to Example 6-8, page 221               During a throttling process, the enthalpy of a
                                              fluid remains constant. But internal and flow
                                              energies may be converted to each other.
                                                                                KEITH VAUGH
Mixing chambers
In engineering applications, the section            60°C

where the mixing process takes place is
commonly referred to as a mixing
chamber.
                                                               140 kPa


                                                   10°C                     43°C



                                             Energy balance for the adiabatic
                                             mixing chamber in the figure

                                                  & &
                                                  Ein = Eout
                                                  &      &       &
                                                  m1h1 + m2 h2 = m3h3
     The T-elbow of an ordinary              Since
     shower serves as the mixing              &      &
                                             Q ≅ 0, W ≅ 0, Δke ≅ 0 and        Δpe ≅ 0
     chamber for the hot and the
     cold-water streams.


                                           Refer to Example 6-9, page 223     KEITH VAUGH
Heat exchangers
  Heat exchangers are devices where two
  moving fluid streams exchange heat without
  mixing. Heat exchangers are widely used in
  various industries and come in a variety of
  designs.


                                                A heat exchanger can be as simple
                                                as two concentric pipes




      The heat transfer
 associated with a heat
exchanger may be zero
 or nonzero depending
    on how the control
    volume is selected.
                                                                              KEITH VAUGH
Mass and energy balances for the
adiabatic heat exchanger in the
figure are:

      & &
      Ein = Eout
       & & &
       m1 = m2 = mW
       & & &
       m3 = m4 = m R
      &      &      &       &
      m1h1 + m3h3 = m2 h2 + m4 h4




      Refer to Example 6-10, page 224   KEITH VAUGH
Pipe and duct flow
The transport of liquids or gases in pipes
and ducts is of great importance in many
engineering applications. Flow through a
pipe or a duct usually satisfies the steady-
flow conditions.




Heat losses from a hot fluid flowing through        Pipe or duct flow may involve more
an uninsulated pipe or duct to the cooler     than one form of work at the same time.
environment may be very significant.




                                                                             KEITH VAUGH
Energy balance for the pipe flow
   shown in the figure is


        & &
        Ein = Eout
         &       &      &      &
        We, in + m1h1 = Qout + m2 h2
         &       &      &
        We, in − Qout = m1c p (T2 − T1 )




Refer to Example 6-11, page 227   KEITH VAUGH
ENERGY ANALYSIS OF
UNSTEADY FLOW PROCESSES
   Many processes of interest, however, involve
   changes within the control volume with time. Such
   processes are called unsteady-flow, or transient-flow,
   processes.
                                                          }
   Most unsteady-flow processes can be represented
   reasonably well by the uniform-flow process.

   Uniform-flow process
    The fluid flow at any inlet or exit is uniform and
   steady, and thus the fluid properties do not change
   with time or position over the cross section of an
   inlet or exit. If they do, they are averaged and
   treated as constants for the entire process.

                                                          KEITH VAUGH
Charging of a rigid tank from a supply
line is an unsteady-flow process since
it involves changes within the control
volume.


                                         KEITH VAUGH
Charging of a rigid tank from a supply
line is an unsteady-flow process since
it involves changes within the control
volume.


                                         KEITH VAUGH
Charging of a rigid tank from a supply   The shape and size of a control volume
line is an unsteady-flow process since      may change during an unsteady-flow
it involves changes within the control                                 process.
volume.


                                                                       KEITH VAUGH
Mass balance
   & &           &
   min − mout = Δmsystem

    &
   Δmsystem = m final − minitial

                                   {
                                       i = inlet
                                       e = exit
   mi − me = ( m2 − m1 )CV             1 = initial state
                                       2 = final state




                                                           KEITH VAUGH
Mass balance
    & &           &
    min − mout = Δmsystem

     &
    Δmsystem = m final − minitial

                                                   {
                                                                    i = inlet
                                                                    e = exit
    mi − me = ( m2 − m1 )CV                                         1 = initial state
                                                                    2 = final state

Energy balance
    Ein − Eout            =               Esystem
    14 2 4 3                              {
   Net energy transfer               Change in internal,
 by heat, work and mass       kinetic, potential, etc... energies




                                                                                        KEITH VAUGH
Mass balance
    & &           &
    min − mout = Δmsystem

     &
    Δmsystem = m final − minitial

                                                   {
                                                                    i = inlet
                                                                    e = exit
    mi − me = ( m2 − m1 )CV                                         1 = initial state
                                                                    2 = final state

Energy balance
    Ein − Eout            =               Esystem
    14 2 4 3                              {
   Net energy transfer               Change in internal,
 by heat, work and mass       kinetic, potential, etc... energies


    ⎛                  ⎞ ⎛                      ⎞
    ⎜ Qin + Win + ∑ mθ ⎟ − ⎜ Qout + Wout + ∑ mθ ⎟ = ( m2 e2 − m1e1 )system
    ⎝                  ⎠ ⎝                      ⎠
                   in                         out




                                                                                        KEITH VAUGH
Mass balance
    & &           &
    min − mout = Δmsystem

     &
    Δmsystem = m final − minitial

                                                   {
                                                                    i = inlet
                                                                    e = exit
    mi − me = ( m2 − m1 )CV                                         1 = initial state
                                                                    2 = final state

Energy balance
    Ein − Eout            =               Esystem
    14 2 4 3                              {
   Net energy transfer               Change in internal,
 by heat, work and mass       kinetic, potential, etc... energies


    ⎛                  ⎞ ⎛                      ⎞
    ⎜ Qin + Win + ∑ mθ ⎟ − ⎜ Qout + Wout + ∑ mθ ⎟ = ( m2 e2 − m1e1 )system
    ⎝                  ⎠ ⎝                      ⎠
                   in                         out

    θ = h + ke + pe
    e = u + ke + pe


                                                                                        KEITH VAUGH
The energy equation of a uniform-flow system
reduces to that of a closed system when all
the inlets and exits are closed.




                                              KEITH VAUGH
The energy equation of a uniform-flow system
reduces to that of a closed system when all
the inlets and exits are closed.




                                              KEITH VAUGH
The energy equation of a uniform-flow system       A uniform flow system may involve
reduces to that of a closed system when all   electrical, shaft and boundary work all
the inlets and exits are closed.                                             at once




                                                                             KEITH VAUGH
Conservation of mass
    Mass and volume flow rates
    Mass balance for a steady flow process
    Mass balance for incompressible flow
Flow work and the energy of a flowing fluid
    Energy transport by mass
Energy analysis of steady flow systems
Steady flow engineering devices
    Nozzles and diffusers
    Turbines and compressors
    Throttling valves
    Mixing chambers and heat exchangers
    Pipe and duct flow
Energy analysis of unsteady flow processes

                                             KEITH VAUGH

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SSL8 Mass & Energy Analysis of Control Systems

  • 1. MASS & ENERGY ANALYSIS OF CONTROL SYSTEMS Lecture 8 Keith Vaugh BEng (AERO) MEng Reference text: Chapter 6 - Fundamentals of Thermal-Fluid Sciences, 3rd Edition Yunus A. Cengel, Robert H. Turner, John M. Cimbala McGraw-Hill, 2008 KEITH VAUGH
  • 2. OBJECTIVES } KEITH VAUGH
  • 3. OBJECTIVES Develop the conservation of mass principle. } KEITH VAUGH
  • 4. OBJECTIVES Develop the conservation of mass principle. Apply the conservation of mass principle to various systems including steady- and unsteady-flow control } volumes. KEITH VAUGH
  • 5. OBJECTIVES Develop the conservation of mass principle. Apply the conservation of mass principle to various systems including steady- and unsteady-flow control } volumes. Apply the first law of thermodynamics as the statement of the conservation of energy principle to control volumes. KEITH VAUGH
  • 6. OBJECTIVES Develop the conservation of mass principle. Apply the conservation of mass principle to various systems including steady- and unsteady-flow control } volumes. Apply the first law of thermodynamics as the statement of the conservation of energy principle to control volumes. Identify the energy carried by a fluid stream crossing a control surface as the sum of internal energy, flow work, kinetic energy, and potential energy of the fluid and to relate the combination of the internal energy and the flow work to the property enthalpy. KEITH VAUGH
  • 8. Solve energy balance problems for common steady-flow devices such as nozzles, compressors, turbines, throttling valves, mixers, heaters, and heat exchangers. } KEITH VAUGH
  • 9. Solve energy balance problems for common steady-flow devices such as nozzles, compressors, turbines, throttling valves, mixers, heaters, and heat exchangers. } Apply the energy balance to general unsteady-flow processes with particular emphasis on the uniform-flow process as the model for commonly encountered charging and discharging processes. KEITH VAUGH
  • 10. CONSERVATION OF MASS Conservation of mass } Mass, like energy, is a conserved property, and it cannot be created or destroyed during a process. Closed systems The mass of the system remain constant during a process. Control volumes Mass can cross the boundaries, and so we must keep track of the amount of mass entering and leaving the control volume. KEITH VAUGH
  • 11. Mass is conserved even during chemical reactions KEITH VAUGH
  • 12. Mass is conserved even during chemical reactions Mass m and energy E can be converted to each other according to E = mc 2 where c is the speed of light in a vacuum, which is c = 2.9979 × 108 m/s. The mass change due to energy change is absolutely negligible. KEITH VAUGH
  • 13. MASS & VOLUME FLOW RATES & δ m = ρVn dAc & & m = ∫ δ m = ∫ ρVn dAc Ac Ac } 1 Definition of Vavg = ∫ Vn dAc Ac Ac average velocity The average velocity Vavg is defined as the average speed through a cross section. KEITH VAUGH
  • 14. MASS & VOLUME FLOW RATES & δ m = ρVn dAc & & m = ∫ δ m = ∫ ρVn dAc Ac Ac } 1 Definition of Vavg = ∫ Vn dAc Ac Ac average velocity The average velocity Vavg is defined as the average speed through a cross section. & m = ρVavg Ac ( s) kg KEITH VAUGH
  • 15. MASS & VOLUME FLOW RATES & δ m = ρVn dAc & & m = ∫ δ m = ∫ ρVn dAc Ac Ac } 1 Definition of Vavg = ∫ Vn dAc Ac Ac average velocity The average velocity Vavg is defined as the average speed through a cross section. & m = ρVavg Ac ( s) kg & V & & m = ρV = Mass flow rate v KEITH VAUGH
  • 16. MASS & VOLUME FLOW RATES & δ m = ρVn dAc & & m = ∫ δ m = ∫ ρVn dAc Ac Ac } 1 Definition of Vavg = ∫ Vn dAc Ac Ac average velocity The average velocity Vavg is defined as the average speed through a cross section. & m = ρVavg Ac ( s) kg & V & & m = ρV = Mass flow rate v Volume flow rate & V = ∫ Vn dAc = Vavg Ac = VAc Ac ( s) m3 KEITH VAUGH
  • 17. MASS & VOLUME FLOW RATES & δ m = ρVn dAc & & m = ∫ δ m = ∫ ρVn dAc Ac Ac } 1 Definition of Vavg = ∫ Vn dAc Ac Ac average velocity The average velocity Vavg is defined as the average speed through a cross section. & m = ρVavg Ac ( s) kg & V & & m = ρV = Mass flow rate v Volume flow rate & V = ∫ Vn dAc = Vavg Ac = VAc Ac ( s) m3 The volume flow rate is the volume of fluid flowing through a cross section per unit time. KEITH VAUGH
  • 18. CONSERVATION OF MASS PRINCIPLE The conservation of mass principle for a control volume The net mass transfer to or from a control volume during a time interval Δt is equal to the net change (increase or decrease) in } the total mass within the control volume during Δt. ⎛ Total mass entering ⎞ ⎛ Total mass leaving ⎞ ⎛ Net change in mass ⎞ ⎜ the CV during Δt ⎟ − ⎜ the CV during Δt ⎟ = ⎜ within the CV during Δt ⎟ ⎝ ⎠ ⎝ ⎠ ⎝ ⎠ KEITH VAUGH
  • 19. min − mout = Δmcv ( kg ) dmcv & & min − mout = dt ( s) kg Conservation of mass principle for an ordinary bathtub KEITH VAUGH
  • 20. min − mout = Δmcv ( kg ) dmcv & & min − mout = dt ( s) kg General conservation of mass d r r dt ∫ cv ρ dV + ∫ cs ( ) ρ V ⋅ n dA = 0 Conservation of mass principle for an ordinary bathtub KEITH VAUGH
  • 21. min − mout = Δmcv ( kg ) dmcv & & min − mout = dt ( s) kg General conservation of mass d r r dt ∫ cv ρ dV + ∫ cs ( ) ρ V ⋅ n dA = 0 General conservation of mass in rate form d ∫ & & ρ dV = ∑ m − ∑ m dt cv in out Conservation of mass principle for an ordinary bathtub dmcv or & = ∑m − ∑m & dt in out KEITH VAUGH
  • 22. MASS BALANCE FOR STEADY FLOW PROCESSES During a steady-flow process, the total amount of mass contained within a control volume does not change with time (mCV = constant). } Then the conservation of mass principle requires that the total amount of mass entering a control volume equal the total amount of mass leaving it. KEITH VAUGH
  • 23. For steady-flow processes, we are interested in the amount of mass flowing per unit time, that is, the mass flow rate & in & ∑m = ∑m out ( s) kg Multiple inlets and exits & & m1 = m2 → ρV1 A1 = ρV2 A2 Single stream Many engineering devices such as nozzles, diffusers, turbines, compressors, and pumps involve a single stream (only one inlet and one Conservation of mass principle for a two outlet). inlet - one outlet steady flow system KEITH VAUGH
  • 24. Special case: Incompressible Flow The conservation of mass relations can be simplified even further when the fluid is incompressible, which is usually the case for liquids. & & ∑V = ∑V in out ( s) m3 & & V1 = V2 → V1 A1 = V2 A2 There is no such thing as a “conservation of volume” principle. However, for steady flow of liquids, the volume flow rates, as well as the mass flow rates, remain constant since liquids are essentially During a steady-flow process, incompressible substances. volume flow rates are not necessarily conserved although mass flow rates are. KEITH VAUGH
  • 25. FLOW WORK & THE ENERGY OF A FLOWING FLUID Flow work, or flow energy The work (or energy) required to push the mass into or out of the control volume. This work is necessary for maintaining a continuous flow through a control volume. } In the absence of acceleration, the force applied on a fluid by a piston is equal to the force applied on the piston by the fluid. KEITH VAUGH
  • 26. FLOW WORK & THE ENERGY OF A FLOWING FLUID Flow work, or flow energy The work (or energy) required to push the mass into or out of the control volume. This work is necessary for maintaining a continuous flow through a control volume. } In the absence of acceleration, the force applied on a fluid by a piston is equal to the force applied on the piston by the fluid. KEITH VAUGH
  • 27. F = PA W flow = FL = PAL = PV ( kJ ) W flow = Pv ( kg) kJ Schematic for flow work KEITH VAUGH
  • 28. TOTAL ENERGY OF A FLOWING FLUID e = u + ke + pe = u + V2 2 + gz ( kg) kJ } θ = Pv + e = Pv + ( u + ke + pe) KEITH VAUGH
  • 29. TOTAL ENERGY OF A FLOWING FLUID e = u + ke + pe = u + V2 2 + gz ( kg) kJ } θ = Pv + e = Pv + ( u + ke + pe) But the combination Pv + u has been previously defined as the enthalpy h KEITH VAUGH
  • 30. TOTAL ENERGY OF A FLOWING FLUID e = u + ke + pe = u + V2 2 + gz ( kg) kJ } θ = Pv + e = Pv + ( u + ke + pe) But the combination Pv + u has been previously defined as the enthalpy h The flow energy is automatically V2 θ = h + ke + pe = h + 2 + gz ( kg) kJ taken care of by enthalpy. In fact, this is the main reason for defining the property enthalpy. KEITH VAUGH
  • 31. The total energy consists of three parts for a non-flowing fluid and four parts for a flowing fluid. KEITH VAUGH
  • 32. ENERGY TRANSPORT BY MASS Amount of energy transport Emass ⎛ = mθ = m ⎜ h + ⎝ V2 2 ⎞ + gz ⎟ ⎠ ( kJ ) } Rate of energy transport & ⎛ V2 ⎞ Emass & & = mθ = m ⎜ h + + gz ⎟ ( kW ) ⎝ 2 ⎠ The product ṁiθi is the energy transported into control volume by mass per unit time KEITH VAUGH
  • 33. When the kinetic and potential energies of a fluid stream are negligible Emass = mh & & Emass = mh The product ṁiθi is the energy When the properties of the mass at transported into control volume by each inlet or exit change with time mass per unit time. as well as over the cross section ⎛ Vi 2 ⎞ Ein,mass = ∫ θ i δ mi = ∫ ⎜ hi + + gzi ⎟ δ mi mi mi ⎝ 2 ⎠ KEITH VAUGH
  • 34. ENERGY TRANSPORT BY MASS Many engineering systems such as power plants operate under steady conditions. } KEITH VAUGH
  • 35. Under steady-flow conditions, the mass Under steady-flow conditions, the fluid and energy contents of a control volume properties at an inlet or exit remain remain constant. constant (do not change with time). KEITH VAUGH
  • 36. Mass and energy balances for a steady-flow process & & ∑m = ∑m in out & & m1 = m2 Mass ρ1V1 A1 = ρ2V2 A2 balance A water heater in steady operation. KEITH VAUGH
  • 37. Mass and energy balances for a steady-flow process & & ∑m = ∑m in out & & m1 = m2 Mass ρ1V1 A1 = ρ2V2 A2 balance Energy balances Z 0 dEsystem & & Ein − Eout = =0 14 2 4 3 dt 3 Rate of net energy transfer 14 2 4 by heat, work and mass Rate of change in internal, kinetic, potential, etc... energies A water heater in steady operation. KEITH VAUGH
  • 38. Mass and energy balances for a steady-flow process & & ∑m = ∑m in out & & m1 = m2 Mass ρ1V1 A1 = ρ2V2 A2 balance Energy balances Z 0 dEsystem & & Ein − Eout = =0 14 2 4 3 dt 3 Rate of net energy transfer 14 2 4 by heat, work and mass Rate of change in internal, kinetic, potential, etc... energies A water heater in steady operation. & Ein = & Eout ( kW ) { { Rate of net energy transfer Rate of net energy out, by heat, work and mass by heat, work and mass KEITH VAUGH
  • 39. Mass and energy balances for a steady-flow process & & ∑m = ∑m in out & & m1 = m2 Mass ρ1V1 A1 = ρ2V2 A2 balance Energy balances Z 0 dEsystem & & Ein − Eout = =0 14 2 4 3 dt 3 Rate of net energy transfer 14 2 4 by heat, work and mass Rate of change in internal, kinetic, potential, etc... energies A water heater in steady operation. & Ein = & Eout ( kW ) { { Rate of net energy transfer Rate of net energy out, by heat, work and mass by heat, work and mass ⎛ & + Win + ∑ m h + & V2 ⎞ & ⎛ & + ∑m h + V2 ⎞ Qin &⎜ + gz ⎟ = Qout + Wout &⎜ + gz ⎟ ⎝ 2 ⎠ ⎝ 2 ⎠ 1 4 44 2 4 4 4 in 3 1 4 44 2 4 4 4 out 3 for each inlet for each exit KEITH VAUGH
  • 40. Energy balance relations with sign conventions (i.e., heat input and work output are positive) ⎛ &− W = + ∑ m h + & V2 ⎞ ⎛ V2 ⎞ Q &⎜ & + gz ⎟ − ∑ m ⎜ h + + gz ⎟ ⎝ 2 ⎠ in ⎝ 2 ⎠ 1 4 44 2 4 4 4 out 3 1 4 44 2 4 4 4 3 for each exit for each inlet ⎡ &− W = m h2 − h1 + & & V22 − V12 ⎤ Q ⎢ + g ( z2 − z1 ) ⎥ ⎣ 2 ⎦ V22 − V12 q − w = h2 − h1 + + g ( z2 − z1 ) 2 q − w = h2 − h1 Q& q= W& W& w= & m Refer to pages, 212 - 214 KEITH VAUGH
  • 41. STEADY FLOW ENGINEERING DEVICES Many engineering devices operate essentially under the same conditions for long periods of time. The components of a steam power plant (turbines, compressors, heat exchangers, and } pumps), for example, operate nonstop for months before the system is shut down for maintenance. Therefore, these devices can be conveniently analysed as steady-flow devices. A modern land-based gas turbine used for electric power production. This is a General Electric LM5000 turbine. It has a length of 6.2 m, it weighs 12.5 tons, and produces 55.2 MW at 3600 rpm with steam injection. KEITH VAUGH
  • 42. Nozzles and Diffusers Commonly utilised in jet engines, rockets, spacecraft, and even garden hoses. A nozzle is a device that increases the velocity of a fluid at the expense of pressure. A diffuser is a device that increases the pressure of a fluid by slowing it down. The cross-sectional area of a nozzle decreases in the flow direction for subsonic flows and increases for supersonic flows. The reverse is Nozzles and diffusers are shaped so true for diffusers. that they cause large changes in fluid velocities and thus kinetic energies. & & Ein = Eout ⎛ V12 ⎞ ⎛ V22 ⎞ & & & & m ⎜ h1 + ⎟ = m ⎜ h2 + ⎟ Since Q ≅ 0, W ≅ 0, and Δpe ≅ 0 ⎝ 2 ⎠ ⎝ 2 ⎠ Refer to Example 6-4 & 6-5, page 216/7 KEITH VAUGH
  • 43. Turbines and compressors Turbine drives the electric generator in power plants. As the fluid passes through the turbine, work is done against the blades, which are attached to the shaft. The shaft rotates, and the turbine produces work. Compressors, as well as pumps and fans, increase the pressure of a fluid. Work is supplied to these devices from an external source through a rotating shaft. Energy balance for the compressor in this figure: A fan increases the pressure of a gas slightly and is mainly used to mobilise a gas. & & Ein = Eout & & & & Win + mh1 = Qout + mh2 A compressor is capable of compressing the gas to very high pressures. Since Δke = Δpe ≅ 0 Pumps work very much like compressors Refer to Example 6-6 & 6-7, page 218/9 except that they handle liquids instead of gases. KEITH VAUGH
  • 44. Throttling valves Throttling valves are any kind of flow- restricting devices that cause a significant pressure drop in the fluid. The pressure drop in the fluid is often accompanied by a large drop in temperature and for that reason throttling The temperature of an ideal gas does not change during a throttling (h = constant) devices are commonly used in refrigeration process since h = h(T). and air-conditioning applications. h2 ≅ h1 Energy balance u1 + P1v1 = u2 + P2 v2 Internal energy + Flow Energy = Constant Refer to Example 6-8, page 221 During a throttling process, the enthalpy of a fluid remains constant. But internal and flow energies may be converted to each other. KEITH VAUGH
  • 45. Mixing chambers In engineering applications, the section 60°C where the mixing process takes place is commonly referred to as a mixing chamber. 140 kPa 10°C 43°C Energy balance for the adiabatic mixing chamber in the figure & & Ein = Eout & & & m1h1 + m2 h2 = m3h3 The T-elbow of an ordinary Since shower serves as the mixing & & Q ≅ 0, W ≅ 0, Δke ≅ 0 and Δpe ≅ 0 chamber for the hot and the cold-water streams. Refer to Example 6-9, page 223 KEITH VAUGH
  • 46. Heat exchangers Heat exchangers are devices where two moving fluid streams exchange heat without mixing. Heat exchangers are widely used in various industries and come in a variety of designs. A heat exchanger can be as simple as two concentric pipes The heat transfer associated with a heat exchanger may be zero or nonzero depending on how the control volume is selected. KEITH VAUGH
  • 47. Mass and energy balances for the adiabatic heat exchanger in the figure are: & & Ein = Eout & & & m1 = m2 = mW & & & m3 = m4 = m R & & & & m1h1 + m3h3 = m2 h2 + m4 h4 Refer to Example 6-10, page 224 KEITH VAUGH
  • 48. Pipe and duct flow The transport of liquids or gases in pipes and ducts is of great importance in many engineering applications. Flow through a pipe or a duct usually satisfies the steady- flow conditions. Heat losses from a hot fluid flowing through Pipe or duct flow may involve more an uninsulated pipe or duct to the cooler than one form of work at the same time. environment may be very significant. KEITH VAUGH
  • 49. Energy balance for the pipe flow shown in the figure is & & Ein = Eout & & & & We, in + m1h1 = Qout + m2 h2 & & & We, in − Qout = m1c p (T2 − T1 ) Refer to Example 6-11, page 227 KEITH VAUGH
  • 50. ENERGY ANALYSIS OF UNSTEADY FLOW PROCESSES Many processes of interest, however, involve changes within the control volume with time. Such processes are called unsteady-flow, or transient-flow, processes. } Most unsteady-flow processes can be represented reasonably well by the uniform-flow process. Uniform-flow process The fluid flow at any inlet or exit is uniform and steady, and thus the fluid properties do not change with time or position over the cross section of an inlet or exit. If they do, they are averaged and treated as constants for the entire process. KEITH VAUGH
  • 51. Charging of a rigid tank from a supply line is an unsteady-flow process since it involves changes within the control volume. KEITH VAUGH
  • 52. Charging of a rigid tank from a supply line is an unsteady-flow process since it involves changes within the control volume. KEITH VAUGH
  • 53. Charging of a rigid tank from a supply The shape and size of a control volume line is an unsteady-flow process since may change during an unsteady-flow it involves changes within the control process. volume. KEITH VAUGH
  • 54. Mass balance & & & min − mout = Δmsystem & Δmsystem = m final − minitial { i = inlet e = exit mi − me = ( m2 − m1 )CV 1 = initial state 2 = final state KEITH VAUGH
  • 55. Mass balance & & & min − mout = Δmsystem & Δmsystem = m final − minitial { i = inlet e = exit mi − me = ( m2 − m1 )CV 1 = initial state 2 = final state Energy balance Ein − Eout = Esystem 14 2 4 3 { Net energy transfer Change in internal, by heat, work and mass kinetic, potential, etc... energies KEITH VAUGH
  • 56. Mass balance & & & min − mout = Δmsystem & Δmsystem = m final − minitial { i = inlet e = exit mi − me = ( m2 − m1 )CV 1 = initial state 2 = final state Energy balance Ein − Eout = Esystem 14 2 4 3 { Net energy transfer Change in internal, by heat, work and mass kinetic, potential, etc... energies ⎛ ⎞ ⎛ ⎞ ⎜ Qin + Win + ∑ mθ ⎟ − ⎜ Qout + Wout + ∑ mθ ⎟ = ( m2 e2 − m1e1 )system ⎝ ⎠ ⎝ ⎠ in out KEITH VAUGH
  • 57. Mass balance & & & min − mout = Δmsystem & Δmsystem = m final − minitial { i = inlet e = exit mi − me = ( m2 − m1 )CV 1 = initial state 2 = final state Energy balance Ein − Eout = Esystem 14 2 4 3 { Net energy transfer Change in internal, by heat, work and mass kinetic, potential, etc... energies ⎛ ⎞ ⎛ ⎞ ⎜ Qin + Win + ∑ mθ ⎟ − ⎜ Qout + Wout + ∑ mθ ⎟ = ( m2 e2 − m1e1 )system ⎝ ⎠ ⎝ ⎠ in out θ = h + ke + pe e = u + ke + pe KEITH VAUGH
  • 58. The energy equation of a uniform-flow system reduces to that of a closed system when all the inlets and exits are closed. KEITH VAUGH
  • 59. The energy equation of a uniform-flow system reduces to that of a closed system when all the inlets and exits are closed. KEITH VAUGH
  • 60. The energy equation of a uniform-flow system A uniform flow system may involve reduces to that of a closed system when all electrical, shaft and boundary work all the inlets and exits are closed. at once KEITH VAUGH
  • 61. Conservation of mass  Mass and volume flow rates  Mass balance for a steady flow process  Mass balance for incompressible flow Flow work and the energy of a flowing fluid  Energy transport by mass Energy analysis of steady flow systems Steady flow engineering devices  Nozzles and diffusers  Turbines and compressors  Throttling valves  Mixing chambers and heat exchangers  Pipe and duct flow Energy analysis of unsteady flow processes KEITH VAUGH

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  12. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
  13. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
  14. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
  15. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
  16. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
  17. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
  18. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
  19. note the use of symbols here. DON’T confuse Volume (V) and velocity (V)\n
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