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Page 1: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

1

6

Page 2: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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

Page 3: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Specific heats

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

Lect-6

• It takes different amounts of energy to raise the temperature of identical masses of different substances by one degree.

• Therefore, it is desirable to have a property that will enable us to compare the energy storage capabilities of various substances.

• This property is the specific heat.

Page 4: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Specific heats

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

Lect-6

• Specific heat is defined as the energy required to raise the temperature of a unit mass of a substance by one degree.

• In general, this energy depends on how the process is executed.

• There are two kinds of specific heats: specific heat at constant volume, cv and specific heat at constant pressure, cp.

Page 5: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Specific heats

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

Lect-6

m = 1 kgΔT = 1oC

Specific heat = 5 kJ/kgoC

5 kJ

Specific heat is the energy required to raise the temperature of a unit mass of a substance by one degree in a specified way.

Page 6: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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 stationary closed system undergoing a constant-volume process

• The conservation of energy principle for this process can be expressed in the differential form as

duee outin =−δδ

Page 7: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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 equation represents the net amount of energy transferred to the system.

• Thus,

vv

v

Tuc

dudTc

∂∂

=

=

or,

olumeconstant vat

Page 8: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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 heat at constant pressure, cp can be obtained by considering a constant-pressure expansion or compression process.

• It yields,

pp

p

Thc

dhdTc

∂∂

=

=

or,

pressureconstant at

Page 9: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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 system is allowed to expand and the energy for the expansion must also be supplied

• Specific heat of a substance change with temperature.

Page 10: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Specific heats

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

Lect-6

(2)

V = constantm = 1 kgΔT = 1o C

cv = 3.12 kJ/kgoC

P = constantm = 1 kgΔT = 1o C

cp = 5.19 kJ/kgoC

3.12 kJ 5.19 kJ

(1)

cp is always > cv

Page 11: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Specific heats

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

Lect-6

Airm = 1 kg

300 301 K

Airm = 1 kg

1000 1001 K

0.718 kJ 0.855 kJ

The specific heat of a substance changes with temperature.

Page 12: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Energy transfer mechanisms

Energy can cross the system boundaries of 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

Page 13: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Energy transfer by heat

• Heat: the form of energy that is transferred between two systems (or a system 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 system boundary.

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

Lect-6

Page 14: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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 HeatRoom air: 25oC

Temperature difference is the driving force for heat transfer. The larger the temperature difference, the higher is the rate of heat transfer.

Page 15: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Energy transfer by heat

• In thermodynamics, heat refers to heat transfer.

• 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

Page 16: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Energy transfer by heat

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

Lect-6

System boundary

Surrounding air

5 kJ thermal energy

5 kJ Heat

5 kJ thermal energy

Heat

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

Page 17: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Energy transfer by heat

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

Lect-6

System boundary

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

Page 18: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Energy transfer by work

• Any energy interaction of a closed system other than heat is work.

• An energy interaction that is not caused by a temperature difference between a system and its surroundings is work.

• Work is the energy transfer associated with a force acting through a distance.

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

Lect-6

Page 19: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Sign conventions

• Heat transfer to a system and work done by a system are positive; heat transfer from a system and work done on a system are negative.

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

Lect-6

System

Surroundings

QoutQin

WoutWin

Page 20: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Energy transfer by heat and work• Both heat and work are boundary

phenomena.• Systems possess energy, but not heat or

work.• Both are associated with a process, not a

state. Unlike properties, heat or work has no meaning at a state.

• Both are path functions (i.e., their magnitudes depend on the path followed during a process as well as the end states).

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

Lect-6

Page 21: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Path and Point functions• Path functions

– Have inexact differentials, sometimes designated by symbol, δ or đ

– Eg. δQ or đQ and δW or đW instead of dQ and dW

• Point functions– Have exact differentials, designated by

symbol, d– Eg. dP, dV, dT

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

Lect-6

Page 22: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Path and Point functions

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

Lect-6

1

2

1m3 5m3 V

p ΔV=4m3; WA=10 kJ

ΔV=4m3; WB=15 kJ

Process A

Process B

Properties are point functions; but heat and work are path functions.

∫∫ −≠−=

zero isproperty a of

but, 1

2

121

2

12 WWWVVdV δ

Page 23: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Work

• Work done by a system on its surroundings during a process is defined as that interaction whose sole effect external to the system could be viewed as the raising of a mass through a distance against gravity.

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

Lect-6

Page 24: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Work

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

Lect-6

Battery

MotorFan

Surroundings

System boundary

W+ _

Page 25: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Work

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

Lect-6

Battery

Motor

Surroundings

System boundary Pulley

+ _

Weight

Page 26: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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

Page 27: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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 film Electrical work: heating of a resistor

Page 28: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Displacement work

• Moving boundary or displacement work is 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

Page 29: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Displacement work

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

Lect-6

A gas does a differential amount of work δWb as it forces the piston to move by a differential amount ds

A ds

P

F

∫=

===2

1

)(kJPdVW

dVPdsPAdsFW

b

Page 30: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Displacement work

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

Lect-6

The area under the process curve on a P-V diagram is equal, in magnitude, to the work done during a quasi-equilibrium expansion or compression process of a closed system.

dV

P

∫ ∫===2

1

2

1

PdVdAAArea

V2 VV1

P 1

2

dA=P dV

Process path

Page 31: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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

B

C

The boundary work done during a process depends on the path followed as well as the end states.

Page 32: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Displacement work

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

Lect-6

V2 VV1

P

1

2

A

B

Wnet

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

Page 33: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

Displacement work

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

Lect-6

• Displacement work during Various processes:

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

Page 34: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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

VVppdVWV

V

−== ∫−

Page 35: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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

Page 36: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

PVn = constant (Polytropic processes)

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

Lect-6

nVPVP

nVVCW

CVPVP

CPV

dVCVPdVW

nn

nn

n

n

−−

=+−−

=

==

=

==

+−+−

−− ∫∫

11

Now,

)(

11221

11

221

2211

2

1

2

121

V

P1 2n=0

n=∞

PVn =constant

Page 37: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

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

Page 38: In this lecture - NPTELnptel.ac.in/courses/101101001/downloads/Intro-Propulsion-Lect-6.pdfIn this lecture ... • Specific heat – At constant pressure and constant volume • Heat

In the next lecture ...

• Solve problems related to calculation of– Work done (displacement work)

Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay38

Lect-6