intro-propulsion-lect-6.pdf

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    In this lecture ...

    Specific heat At constant pressure and constant

    volume

    Heat transfer Meaning of heat transfer

    Types of heat transfer

    Work Thermodynamic meaning of work

    Different types of work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay2

    Lect-6

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    Specific heats

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay3

    Lect-6

    It takes different amounts of energy toraise the temperature of identical massesof different substances by one degree.

    Therefore, it is desirable to have aproperty that will enable us to comparethe energy storage capabilities of varioussubstances.

    This property is the specific heat.

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    Specific heats

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay4

    Lect-6

    Specific heat is defined as the energyrequired to raise the temperature of aunit mass of a substance by one degree.

    In general, this energy depends on howthe process is executed.

    There are two kinds of specific heats:specific heat at constant volume, cvand

    specific heat at constant pressure, cp.

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    Specific heats

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay5

    Lect-6

    m = 1 kgT = 1oC

    Specific heat = 5 kJ/kgoC

    5 kJ

    Specific heat is the energy required to raise thetemperature of a unit mass of a substance byone degree in a specified way.

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    Specific heat at constant volume

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay6

    Lect-6

    Consider a fixed mass in a stationaryclosed system undergoing a constant-volume process

    The conservation of energy principle forthis process can be expressed in thedifferential form as

    duee outin =

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    Specific heat at constant volume

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay7

    Lect-6

    The left-hand side of this equationrepresents the net amount of energytransferred to the system.

    Thus,

    v

    v

    v

    T

    uc

    dudTc

    =

    =

    or,

    olumeconstant vat

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    Specific heat at constant pressure

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay8

    Lect-6

    Similarly, an expression for the specific heatat constant pressure, cp can be obtained byconsidering a constant-pressure expansionor compression process.

    It yields,

    p

    p

    p

    Thc

    dhdTc

    =

    =

    or,

    pressureconstantat

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    Specific heats

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay9

    Lect-6

    cp and cv are properties of a system.

    Are valid for any processes

    cp

    is always > cv

    Because at constant pressure the systemis allowed to expand and the energy forthe expansion must also be supplied

    Specific heat of a substance change withtemperature.

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    Specific heats

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay10

    Lect-6

    (2)

    V = constantm = 1 kg

    T = 1o C

    cv = 3.12 kJ/kgoC

    P = constantm = 1 kg

    T = 1o C

    cp = 5.19 kJ/kgoC

    3.12 kJ 5.19 kJ

    (1)

    cp is always > cv

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    Specific heats

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay11

    Lect-6

    Air

    m = 1 kg

    300 301 K

    Air

    m = 1 kg

    1000 1001 K

    0.718 kJ 0.855 kJ

    The specific heat of a substancechanges with temperature.

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    Energy transfer mechanisms

    Energy can cross the system boundariesof a closed system: heat and work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay12

    Lect-6

    Closed system(m = constant)

    Heat

    Work

    System boundary

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    Energy transfer by heat

    Heat: the form of energy that istransferred between two systems (or asystem and its surroundings) by virtue of

    a temperature difference. Energy interaction is heat only if it takes

    place by virtue of temperature difference.

    Heat is energy in transition; it is

    recognised only as it crosses the systemboundary.

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay13

    Lect-6

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    Energy transfer by heat

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay14

    Lect-6

    25oC 15oC 5oC

    No heat transfer 8 J/s 18 J/s

    Heat Heat

    Room air: 25oC

    Temperature difference is the driving force forheat transfer. The larger the temperaturedifference, the higher is the rate of heat transfer.

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    Energy transfer by heat

    In thermodynamics, heat refers to heattransfer.

    A process during which there is no heat

    transfer is called Adiabatic process. Heat transfer mechanisms:

    Conduction

    Convection Radiation

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay15

    Lect-6

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    Energy transfer by heat

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay16

    Lect-6

    Systemboundary

    Surrounding air

    5 kJthermalenergy

    5 kJHeat

    5 kJthermalenergy

    Heat

    Energy is recognized as heat transferonly as it crosses the system boundary.

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    Energy transfer by heat

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay17

    Lect-6

    Systemboundary

    Qn. Is there is any heat transfer during this burning process?Qn. Is there is any change in the internal energy of the system?

    Insulation

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    Energy transfer by work

    Any energy interaction of a closedsystem other than heat is work.

    An energy interaction that is not caused

    by a temperature difference between asystem and its surroundings is work.

    Work is the energy transfer associatedwith a force acting through a distance.

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay18

    Lect-6

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    Sign conventions

    Heat transfer to a system and work doneby a system are positive; heat transferfrom a system and work done on a systemare negative.

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay19

    Lect-6

    System

    Surroundings

    QoutQin

    WoutWin

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    Energy transfer by heat and work

    Both heat and work are boundaryphenomena.

    Systems possess energy, but not heat orwork.

    Both are associated with a process, not astate. Unlike properties, heat or work hasno meaning at a state.

    Both are path functions (i.e., theirmagnitudes depend on the path followedduring a process as well as the end states).

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay20

    Lect-6

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    Path and Point functions

    Path functions Have inexact differentials, sometimes

    designated by symbol, or

    Eg. Q or Q and Wor Winstead ofdQ and dW

    Point functions

    Have exact differentials, designated bysymbol, d

    Eg. dP, dV, dT

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay21

    Lect-6

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    Path and Point functions

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay22

    Lect-6

    1

    2

    1m3

    5m3

    V

    pV=4m3; WA=10 kJ

    V=4m3; WB=15 kJ

    Process A

    Process B

    Properties are point functions; butheat and work are path functions.

    =

    zeroispropertyaof

    but, 1

    2

    1

    21

    2

    1

    2 WWWVVdV

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    Work

    Work done by a system on its surroundingsduring a process is defined as thatinteraction whose sole effect external to

    the system could be viewed as the raisingof a mass through a distance againstgravity.

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay23

    Lect-6

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    Work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay24

    Lect-6

    Battery

    MotorFan

    Surroundings

    Systemboundary

    W+

    _

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    Work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay25

    Lect-6

    Battery

    Motor

    Surroundings

    Systemboundary Pulley

    +_

    Weight

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    Work

    Examples: PdV: displacement work

    Electrical work: heating of a resistor

    Shaft work: rotation of a shaft Paddle wheel work

    Spring work

    Stretching of a liquid film

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay26

    Lect-6

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    Work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay27

    Lect-6

    Shaft work: rotation of a shaft Spring work

    Stretching of a liquid filmElectrical work: heating of a resistor

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    Displacement work

    Moving boundary or displacement workis of significant interest to engineers.

    Many engineering systems generate

    useful work output by this mode. Examples: automobile engines, steam

    engines, pumps etc.

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay28

    Lect-6

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    Displacement work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay29

    Lect-6

    A gas does a differential amountof work Wb as it forces thepiston to move by a differential

    amount ds

    A ds

    P

    F

    =

    ===2

    1)(kJPdVW

    dVPdsPAdsFW

    b

    b

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    Displacement work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay30

    Lect-6

    The area under theprocess curve on a P-Vdiagram is equal, inmagnitude, to the work

    done during a quasi-equilibrium expansion orcompression process ofa closed system.

    dV

    P

    ===2

    1

    2

    1

    PdVdAAArea

    V2 VV1

    P 1

    2

    dA=P dV

    Process path

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    Displacement work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay31

    Lect-6

    V2 VV1

    P

    1

    2

    WA = 12 kJWB = 10 kJ

    WC = 7 kJ

    A

    BC

    The boundary work done during a processdepends on the path followed as well as theend states.

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    Displacement work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay32

    Lect-6

    V2 VV1

    P1

    2

    A

    B

    Wnet

    The net work done during a cycle is thedifference between the work done by thesystem and the work done on the system.

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    Displacement work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay33

    Lect-6

    Displacement work during Variousprocesses:

    Constant pressure processConstant volume processPV= contantPolytropic process, PVn = constant

    6

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    Constant pressure process

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay34

    Lect-6

    V2 VV1

    P

    1 2

    W1-2)( 1221

    2

    1

    VVppdVW

    V

    V

    ==

    L 6

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    Constant volume process

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay35

    Lect-6

    V

    P1

    P

    1

    2

    0)( 1221

    2

    1

    === VVppdVWV

    VP2

    L t 6

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    PVn = constant (Polytropic processes)

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay36

    Lect-6

    n

    VPVP

    n

    VVCW

    CVPVPCPV

    dVCVPdVW

    nn

    nn

    n

    n

    =

    +

    =

    ===

    ==

    ++

    11

    Now,)(

    1122

    1

    1

    1

    221

    2211

    2

    1

    2

    1

    21

    V

    P1 2n=0

    n=

    PVn =constant

    L t 6

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    Recap of this lecture

    Specific heat At constant pressure and constant

    volume

    Heat transfer Meaning of heat transfer

    Types of heat transfer

    Work

    Thermodynamic meaning of work

    Different types of work

    Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay37

    Lect-6

    L t 6

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    In the next lecture ...

    Solve problems related to calculation of

    Work done (displacement work)

    38

    Lect-6