solution of problems in heat transfer transient conduction
TRANSCRIPT
1
Solution of Problems in Heat Transfer
Transient Conduction or Unsteady
Conduction
Author
Assistant Professor: Osama Mohammed Elmardi
Mechanical Engineering Department
Faculty of Engineering and Technology
Nile Valley University, Atbara, Sudan
First Edition: April 2017
2
Solution of Problems in Heat Transfer
Transient Conduction or Unsteady
Conduction
Author
Assistant Professor: Osama Mohammed Elmardi
Mechanical Engineering Department
Faculty of Engineering and Technology
Nile Valley University, Atbara, Sudan
First Edition: April 2017
ii
Dedication
In the name of Allah, the merciful, the compassionate
All praise is due to Allah and blessings and peace is upon his messenger and
servant, Mohammed, and upon his family and companions and whoever follows his
guidance until the day of resurrection.
To the memory of my mother Khadra Dirar Taha, my father Mohammed
Elmardi Suleiman, and my dear aunt Zaafaran Dirar Taha who they taught me the
greatest value of hard work and encouraged me in all my endeavors.
To my first wife Nawal Abbas and my beautiful three daughters Roa, Rawan
and Aya whose love, patience and silence are my shelter whenever it gets hard.
To my second wife Limya Abdullah whose love and supplication to Allah were
and will always be the momentum that boosts me through the thorny road of research.
To Professor Mahmoud Yassin Osman for reviewing and modifying the
manuscript before printing process.
This book is dedicated mainly to undergraduate and postgraduate students,
especially mechanical and production engineering students where most of the
applications are of mechanical engineering nature.
To Mr. Osama Mahmoud of Daniya Center for publishing and printing services
whose patience in editing and re β editing the manuscript of this book was the
momentum that pushed me in completing successfully the present book.
To my friend Professor Elhassan Mohammed Elhassan Ishag, Faculty of
Medicine, University of Gezira, Medani, Sudan.
To my friend Mohammed Ahmed Sambo, Faculty of Engineering and
Technology, Nile Valley University, Atbara, Sudan.
iii
To my homeland, Sudan, hoping to contribute in its development and
superiority.
Finally, may Allah accept this humble work and I hope that it will be beneficial
to its readers
iv
Acknowledgement
I am grateful and deeply indebted to Professor Mahmoud Yassin Osman for
valuable opinions, consultation and constructive criticism, for without which this
work would not have been accomplished.
I am also indebted to published texts in thermodynamics and heat and mass
transfer which have been contributed to the author's thinking. Members of
Mechanical Engineering Department at Faculty of Engineering and Technology, Nile
Valley University, Atbara β Sudan, and Sudan University of Science & Technology,
Khartoum β Sudan have served to sharpen and refine the treatment of my topics. The
author is extremely grateful to them for constructive criticisms and valuable
proposals.
I express my profound gratitude to Mr. Osama Mahmoud and Mr. Ahmed
Abulgasim of Daniya Center for Printing and Publishing services, Atbara, Sudan
who they spent several hours in editing, re β editing and correcting the present
manuscript.
Special appreciation is due to the British Council's Library for its quick response
in ordering the requested bibliography, books, reviews and papers.
v
Preface
During my long experience in teaching several engineering subjects I noticed
that many students find it difficult to learn from classical textbooks which are written
as theoretical literature. They tend to read them as one might read a novel and fail to
appreciate what is being set out in each section. The result is that the student ends his
reading with a glorious feeling of knowing it all and with, in fact, no understanding of
the subject whatsoever. To avoid this undesirable end a modern presentation has been
adopted for this book. The subject has been presented in the form of solution of
comprehensive examples in a step by step form. The example itself should contain
three major parts, the first part is concerned with the definition of terms, the second
part deals with a systematic derivation of equations to terminate the problem to its
final stage, the third part is pertinent to the ability and skill in solving problems in a
logical manner.
This book aims to give students of engineering a thorough grounding in the
subject of heat transfer. The book is comprehensive in its coverage without
sacrificing the necessary theoretical details.
The book is designed as a complete course test in heat transfer for degree
courses in mechanical and production engineering and combined studies courses in
which heat transfer and related topics are an important part of the curriculum.
Students on technician diploma and certificate courses in engineering will also find
the book suitable although the content is deeper than they might require.
The entire book has been thoroughly revised and a large number of solved
examples and additional unsolved problems have been added. This book contains
comprehensive treatment of the subject matter in simple and direct language.
The book comprises eight chapters. All chapters are saturated with much needed
text supported and by simple and self-explanatory examples.
Chapter one includes general introduction to transient conduction or unsteady
conduction, definition of its fundamental terms, derivation of equations and a wide
spectrum of solved examples.
vi
In chapter two the time constant and the response of temperature measuring
devices were introduced and discussed thoroughly. This chapter was supported by
different solved examples.
Chapter three discusses the importance of transient heat conduction in solids
with finite conduction and convective resistances. At the end of this chapter a wide
range of solved examples were added. These examples were solved using Heisler
charts.
In chapter four transient heat conduction in semi β infinite solids were
introduced and explained through the solution of different examples using Gaussian
error function in the form of tables and graphs.
Chapter five deals with the periodic variation of surface temperature where the
periodic type of heat flow was explained in a neat and regular manner. At the end of
this chapter a wide range of solved examples was introduced.
Chapter six concerns with temperature distribution in transient conduction. In
using such distribution, the one dimensional transient heat conduction problems could
be solved easily as explained in examples.
In chapter seven additional examples in lumped capacitance system or negligible
internal resistance theory were solved in a systematic manner, so as to enable the
students to understand and digest the subject properly.
Chapter eight which is the last chapter of this book contains unsolved theoretical
questions and further problems in lumped capacitance system. How these problems
are solved will depend on the full understanding of the previous chapters and the
facilities available (e.g. computer, calculator, etc.). In engineering, success depends
on the reliability of the results achieved, not on the method of achieving them.
I would like to express my appreciation of the assistance which I have received
from my colleagues in the teaching profession. I am particularly indebted to Professor
Mahmoud Yassin Osman for his advice on the preparation of this textbook.
When author, printer and publisher have all done their best, some errors may
still remain. For these I apologies and I will be glad to receive any correction or
constructive criticism.
vii
Assistant Professor/ Osama Mohammed Elmardi Suleiman
Mechanical Engineering Department
Faculty of Engineering and Technology
Nile Valley University, Atbara, Sudan
February 2017
viii
Contents
Subject Page
Number
Dedication ii
Acknowledgement iv
Preface v
Contents viii
CHAPTER ONE : Introduction
1.1 General Introduction 2
1.2 Definition of Lumped Capacity or Capacitance System 3
1.3 Characteristic Linear Dimensions of Different Geometries 3
1.4 Derivations of Equations of Lumped Capacitance System 5
1.5 Solved Examples 7
CHAPTER TWO : Time Constant and Response of Temperature
Measuring Instruments
2.1 Introduction 17
2.2 Solved Examples 18
CHAPTER THREE : Transient Heat Conduction in Solids with Finite
Conduction and Convective Resistances
3.1 Introduction 25
3.2 Solved Examples 26
CHAPTER FOUR : Transient Heat Conduction in Semi β Infinite Solids
4.1 Introduction 38
4.2 Penetration Depth and Penetration Time 42
4.3 Solved Examples 43
CHAPTER FIVE : Systems with Periodic Variation of Surface Temperature
5.1 Introduction 51
5.2 Solved Examples 53
ix
CHAPTER SIX : Transient Conduction with Given Temperatures
6.1 Introduction 55
6.2 Solved Examples 55
CHAPTER SEVEN : Additional Solved Examples in Lumped Capacitance
System
7.1 Example (1) Determination of Temperature and Rate of Cooling
of a Steel Ball
58
7.2 Example (2) Calculation of the Time Required to Cool a Thin
Copper Plate
59
7.3 Example (3) Determining the Conditions Under which the
Contact Surface Remains at Constant Temperature
62
7.4 Example (4) Calculation of the Time Required for the Plate to
Reach a Given Temperature
63
7.5 Example (5) Determination of the Time Required for the Plate to
Reach a Given Temperature
64
7.6 Example (6) Determining the Temperature of a Solid Copper
Sphere at a Given Time after the Immersion in a Well β Stirred Fluid
65
7.7 Example (7) Determination of the Heat Transfer Coefficient 66
7.8 Example (8) Determination of the Heat Transfer Coefficient 67
7.9 Example (9) Calculation of the Initial Rate of Cooling of a Steel
Ball
69
7.10 Example (10) Determination of the Maximum Speed of a
Cylindrical Ingot Inside a Furnace
70
7.11 Example (11) Determining the Time Required to Cool a Mild
Steel Sphere, the Instantaneous Heat Transfer Rate, and the Total
Energy Transfer
71
7.12 Example (12) Estimation of the Time Required to Cool a
Decorative Plastic Film on Copper Sphere to a Given Temperature
using Lumped Capacitance Theory
73
x
7.13 Example (13) Calculation of the Time Taken to Boil an Egg 75
7.14 Example (14) Determining the Total Time Required for a
Cylindrical Ingot to be Heated to a Given Temperature
76
CHAPTER EIGHT : Unsolved Theoretical Questions and Further Problems
in Lumped Capacitance System
8.1 Theoretical Questions 80
8.2 Further Problems 80
References 86
Appendix: Mathematical Formula Summary 89
1
Chapter One
Introduction
From the study of thermodynamics, you have learned that energy can be
transferred by interactions of a system with its surroundings. These interactions are
called work and heat. However, thermodynamics deals with the end states of the
process during which an interaction occurs and provides no information concerning
the nature of the interaction or the time rate at which it occurs. The objective of this
textbook is to extend thermodynamic analysis through the study of transient
conduction heat transfer and through the development of relations to calculate
different variables of lumped capacitance theory.
In our treatment of conduction in previous studies we have gradually considered
more complicated conditions. We began with the simple case of one dimensional,
steady state conduction with no internal generation, and we subsequently considered
more realistic situations involving multidimensional and generation effects. However,
we have not yet considered situations for which conditions change with time.
We now recognize that many heat transfer problems are time dependent. Such
unsteady, or transient problems typically arise when the boundary conditions of a
system are changed. For example, if the surface temperature of a system is altered,
the temperature at each point in the system will also begin to change. The changes
will continue to occur until a steady state temperature distribution is reached.
Consider a hot metal billet that is removed from a furnace and exposed to a cool air
stream. Energy is transferred by convection and radiation from its surface to the
surroundings. Energy transfer by conduction also occurs from the interior of the
metal to the surface, and the temperature at each point in the billet decreases until a
steady state condition is reached. The final properties of the metal will depend
significantly on the time β temperature history that results from heat transfer.
Controlling the heat transfer is one key to fabricating new materials with enhanced
properties.
2
Our objective in this textbook is to develop procedures for determining the time
dependence of the temperature distribution within a solid during a transient process,
as well as for determining heat transfer between the solid and its surroundings. The
nature of the procedure depends on assumptions that may be made for the process. If,
for example, temperature gradients within the solid may be neglected, a
comparatively simple approach, termed the lumped capacitance method or negligible
internal resistance theory, may be used to determine the variation of temperature with
time.
Under conditions for which temperature gradients are not negligible, but heat
transfer within the solid is one dimensional, exact solution to the heat equation may
be used to compute the dependence of temperature on both location and time. Such
solutions are for finite and infinite solids. Also, the response of a semi β infinite solid
to periodic heating conditions at its surface is explored.
1.1 General Introduction:
Transient conduction is of importance in many engineering aspects for an
example, when an engine is started sometime should elapse or pass before steady
state is reached. What happens during this lap of time may be detrimental. Again,
when quenching a piece of metal, the time history of the temperature should be
known (i.e. the temperature β time history). One of the cases to be considered is when
the internal or conductive resistance of the body is small and negligible compared to
the external or convective resistance.
This system is also called lumped capacity or capacitance system or negligible
internal resistance system because internal resistance is small, conductivity is high
and the rate of heat flow by conduction is high and therefore, the variation in
temperature through the body is negligible. The measure of the internal resistance is
done by the Biot (Bi) number which is the ratio of the conductive to the convective
resistance.
π. π. π΅π = βπ
π
3
When π΅π βͺ 0.1 the system can be assumed to be of lumped capacity (i.e. at Bi =
0.1 the error is less than 5% and as Bi becomes less the accuracy increases).
1.2 Definition of Lumped Capacity or Capacitance System:
Is the system where the internal or conductive resistance of a body is very small
or negligible compared to the external or convective resistance.
Biot number (Bi): is the ratio between the conductive and convective resistance.
π΅π = βπ
π β π΅π =
πππππ’ππ‘πππ πππ ππ π‘ππππ
ππππ£πππ‘πππ πππ ππ π‘ππππ=
π₯
ππ΄/
1
βπ΄=
π₯
ππ΄Γ
βπ΄
1=
βπ₯
π
Where π₯ is the characteristic linear dimension and can be written as π, β is the heat
transfer coefficient by convection and k is the thermal conductivity.
When π΅π βͺ 0.1 , the system is assumed to be of lumped capacity.
1.3 Characteristic Linear Dimensions of Different Geometries:
The characteristic linear dimension of a body, L = V
Aπ =
volume of the box
surface area of the body
Characteristic linear dimension of a plane surface, L = t
2
Characteristic linear dimension of a cylinder, L = r
2
Characteristic linear dimension of a sphere (ball), L = r
3
Characteristic linear dimension of a cube, L = a
6
Where: t is the plate thickness, r is the radius of a cylinder or sphere, and a is the
length side of a cube.
The derivations of the above characteristic lengths are given below:
i) The characteristic length of plane surface, πΏ =π‘
2
4
π = πππ‘
π΄π = 2ππ‘ + 2ππ‘ + 2ππ
Since, t is very small; therefore, it can be neglected.
π΄π = 2ππ
πΏ =π
π΄π =
πππ‘
2ππ=
π‘
2
ii) The characteristic length of cylinder,
πΏ =π
π΄π =
π
2
π = ππ2πΏ
π΄π = 2πππΏ
β΄ πΏ =π
π΄π =
ππ2πΏ
2πππΏ=
π
2
iii) The characteristic length of a sphere (ball),
πΏ =π
3
π£ =4
3ππ3
π΄π = 4ππ2
β΄ πΏ =π
π΄π =
43
ππ3
4ππ2=
π
3
iv) The characteristic length of a cube,
πΏ =π
6
π = π3
5
π΄π = 6π2
πΏ =π
π΄π =
π3
6π2=
π
6
1.4 Derivation of Equations of Lumped Capacitance System:
Consider a hot body of an arbitrary shape as shown in Fig. (1.1) below:
Energy balance at any instant requires that:
The rate of loss of internal energy of the body must be equal to the rate of convection
from the body to the surrounding fluid.
Fig. (1.1) Hot body of an arbitrary shape
q = βππππ
ππ(π‘)
ππ= βπ΄π (π(π‘) β πβ) (1.1)
Put (π(π‘) β πβ) = π
And,
ππ(π‘)
ππ=
ππ
ππ
β΄ βΟVππ
ππ
ππ= β π΄π π (1.2)
6
If the temperature of the body at time π = 0 is equal to ππ
β΄ ππ = ππ β πβ
βππππ
ππ
π= βπ΄π ππ (1.3)
By integrating the above equation (1.3) we obtain the following equation:
βππππ β«ππ
π= β« βπ΄π ππ
π=π
π=0
π
ππ
βππ lnπ
ππ= βπ΄π π
lnπ
ππ= β
βπ΄π π
ππππ
β΄ π
ππ= π
ββπ΄π πππππ (1.4)
βπ΄π
ππππβ π can be written as
β π
ππ΄π β
π΄π 2π
π2ππππ (1.5)
π
ππππΏ2β π = Fourier number Fo (dimensionless Quantity) (1.6)
And,
β πΏ
π= π΅π (1.7)
β΄ βπ΄π
ππππβ π = π΅π Γ πΉπ (1.8)
β΄ π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ (1.9)
The instantaneous heat transfer rate πβ²(π) is given by the following equation:
πβ²(π) = βπ΄π π = βπ΄π πππβπ΅πΓπΉπ (1.10)
At time π = 0,
7
πβ²(π) = βπ΄π ππ (1.11)
The total heat transfer rate from π = 0 to π = π is given by the following equation:
π(π‘) = β« πβ²(π) = β« βπ΄π πππβπ΅πΓπΉππ
0
π=π
π=0
(1.12)
From equation (1.8) β π΅π Γ πΉπ =βπ΄π
ππππβ π and substitute in equation (1.12), the
following equation is obtained:
π(π‘) = βπ΄π ππ β« πββπ΄π ππππ
βππ
0
= βπ΄π ππ [π
ββπ΄π ππππ
βπ
ββπ΄π ππππ
]
π
= βπ΄π ππ πββπ΄π ππππ
βπΓ
βππππ
βπ΄π = ββπ΄π ππ
ππππ
βπ΄π [π
ββπ΄π ππππ
βπ]
π
π
= ββπ΄π ππ
ππππ
βπ΄π π
ββπ΄π ππππ
βπβ {ββπ΄π ππ
ππππ
βπ΄π }
= ββπ΄π ππ
ππππ
βπ΄π π
ββπ΄π ππππ
βπ+ βπ΄π ππ
ππππ
βπ΄π
= βπ΄π ππ
ππππ
βπ΄π {1 β π
ββπ΄π ππππ
βπ}
= βπ΄π ππ βπ
π΅π Γ πΉπ{1 β πβπ΅πΓπΉπ} (1.13)
1.5 Solved Examples:
Example (1):
Chromium steel ball bearing (π = 50π€/ππΎ, πΌ = 1.3 Γ 10β5π2/π ) are to be heat
treated. They are heated to a temperature of 650ππΆ and then quenched in oil that is at
a temperature of 55ππΆ.
The ball bearings have a diameter of 4cm and the convective heat transfer coefficient
between the bearings and oil is 300π€/π2πΎ. Determine the following:
8
(a) The length of time that the bearings must remain in oil before the temperature
drops to200ππΆ.
(b) The total heat removed from each bearing during this time interval.
(c) Instantaneous heat transfer rate from the bearings when they are first placed in the
oil and when they reach 200ππΆ.
Solution:
Chromium steel ball bearings
π = 50π€/ππΎ
πΌ = π‘βπππππ πππππ’π ππ£ππ‘π¦ = 1.3 Γ 10β5π2/π
ππ = 650ππΆ, πβ = 55ππΆ
Diameter of ball bearing, π = 4ππ = 0.04π
β = 300π€/π2πΎ
a) π = ? π(π‘) = 200ππΆ
π΅π = β πΏ
π
Characteristic length, πΏ =volume of the ball
surface area of the ball=
π
π΄π
β΄ πΏ =π£
π΄π =
43
ππ3
4ππ2=
π
3
π΅π = β πΏ
π=
300 Γ 0.04
6 Γ 50= 0.04
Since π΅π βͺ 0.1 , the lumped capacity system or the negligible internal resistance
theory is valid.
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅π πΉπ
πΉπ =π
ππππΏ2β π =
πΌ
πΏ2β π =
1.3 Γ 10β5
(0.02
3 )2 = 0.2925 π
π
ππ=
200 β 55
650 β 55= πβ0.04Γ0.2925 π
9
0.2437 = πβ0.0117 π
log 0.2437 = log πβ0.0117 π = β0.0117 π log π
β΄ π =log 0.2437
log π Γ β0.0117=
log 0.2437
β0.0117 log π= 120.7 π
b) Q (t) =?
π(π‘) = βπ΄π ππ[1 β πβπ΅πΓπΉπ]π
π΅π Γ πΉπ
π(π‘) = 300 Γ 4π Γ 0.022(650 β 55)[1 β πβ0.04Γ0.2925Γ120.7]120.7
0.04 Γ 0.2925 Γ 120.7
π(π‘) = 58005.4 π½ β 58 ππ
c) Instantaneous heat transfer rate, πβ²(π) = ?
i) When they are first placed in oil,
πβ²(π) = βπ΄π ππ = 300 Γ 4π Γ 0.022(650 β 55) = 897.24π€
ii) When they reach 200ππ,
πβ²(π) = βπ΄π πππβπ΅πΓπΉπ = 897.24 Γ πβ0.04Γ0.2925Γ120.7 = 218.6π€
Example (2):
The product from a chemical process is in the form of pellets which are
approximately spherical to the mean diameter, π = 4ππ . These pellets are initially
at 403πΎ and must be cooled to 343πΎ maximum before entering storage vessel. This
proposed to cool these pellets to the required temperature by passing them down
slightly inclined channel where they are subjected to a stream of air at 323K. If the
length of the channel is limited to 3m, calculate the maximum velocity of the pellets
along the channel and the total heat transferred from one pellet.
Heat transfer from pellet surface to the air stream may be considered to be the
limiting process with β π
ππ= 2 .
Where:
β = heat transfer coefficient at the pellet surface.
10
ππ = thermal conductivity of air = 0.13π€/ππΎ
Other data:
Pellet material density = 480ππ/π3
Specific heat capacity ππ = 2ππ/πππΎ
You may assume that the lumped capacitance system theory is applicable.
Solution:
The product from a chemical process in the form of spherical pellets,
π = 4ππ = 0.004π, π = 0.002π
ππ = 403 πΎ
π(π‘) = 343 πΎ
πβ = 323 πΎ
Length of the channel, πΏ = 3π
Calculate:
* The maximum velocity of the pellets along the channel, π£πππ₯ = ?
* π(π‘) = ?
Heat transfer from pellet surface to the air stream is limited to β π
ππ= 2
ππ = 0.13π€/ππΎ
π pellet = 480ππ/π3
ππ = 2ππ/πππΎ = 2 Γ 103π/πππΎ
It is assumed that lumped capacity system or negligible internal resistance theory is
applicable.
Max. Velocity, π£πππ₯ =πΏ
π
Biot Number, π΅π = β πΏ
π
Characteristic length, L,
πΏ =volume of a sphere
surface area of a sphere=
π
π΄π =
43
ππ3
4ππ2=
π
3
β΄ πΏ = π
3=
0.002
3π
11
π΅π = β π
3π=
0.002β
3π
β π
ππ= Ψ 2
β Γ 0.004
0.13= 2
β΄ β = 2 Γ 0.13
0.004= 65π€/π2πΎ
π΅π =0.002 Γ 65
3π=
0.13
3π
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓ πΉπ
π
ππ=
343 β 323
403 β 323= πβ
0.133π
Γ πΉπ
πΉπ =π
ππππΏ2β π =
π
480 Γ 2 Γ 103 Γ (0.002
3 )2 β π
πΉπ = 2.34375π π
π
ππ= 0.25 = πβ
0.133π
Γ2.34375π π
0.25 = πβ0.1015625 π
log 0.25 = β0.1015625 π log π
β΄ π =log 0.25
log π Γ β0.1015625=
log 0.25
β0.1015625 log π= 13.65 π
β΄ max. velocity, π£πππ₯ =πΏ
π=
3
13.65= 0.22π/π
π(π‘) = βπ΄π ππ[1 β πβπ΅πΓπΉπ]π
π΅π Γ πΉπ
π(π‘) = 65 Γ 4π Γ 0.0022(403 β 323) [1 β πβ0.133π
Γ2.34375πΓ13.65] Γ
12
13.65
0.133
Γ 2.34375 Γ 13.05= 1.93 π½/ pellet
β΄ π(π‘) = 1.93 π½/ pellet
Example (3):
A piece of chromium steel of length 7.4cm (density=8780kg/m3 ; π = 50π€/ππΎ and
specific heat ππ = 440π/πππΎ) with mass 1.27kg is rolled into a solid cylinder and
heated to a temperature of 600oC and quenched in oil at 36oc. Show that the lumped
capacitance system analysis is applicable and find the temperature of the cylinder
after 4min. What is the total heat transfer during this period?
You may take the convective heat transfer coefficient between the oil and cylinder at
280w/m2k.
Solution:
A piece of chromium steel, L = 7.4cm = 0.074m
π = 8780ππ/π3; π = 50π€/ππΎ; ππ = 440π/πππΎ; π = 1.27ππ
Rolled into a solid cylinder,
ππ = 600ππΆ; πβ = 36ππΆ; β = 280π€/π2πΎ
π(π‘) =? πππ‘ππ 4πππ . (π. π. π = 4 Γ 60 = 240π ); π(π‘) =?
π΅π =β πΏ
π
Characteristic length, πΏ =volume of a cylinder
surface area of a cylinder=
π
π΄π
=ππ2πΏ
2πππΏ=
π
2
β΄ π΅π = βπ
2π
π =π
π=
1.27
8780= 1.4465 Γ 10β4π3
13
πΏ = 7.4ππ = 0.074π
π = ππ2πΏ = 1.4465 Γ 10β4
β΄ π = β1.4465 Γ 10β4
π Γ 0.074= 0.025π
π΅π =β π
2π=
280 Γ 0.025
2 Γ 50= 0.07
Since π΅π βͺ 0.1 , then the system is assumed to be of lumped capacitance system,
and therefore the lumped capacitance system analysis or the negligible internal
resistance theory is applicable.
π(π‘) =?
π = 4 Γ 60 = 240 π
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅π πΉπ
πΉπ =π
ππππΏ2β π
πΉπ =50
8780 Γ 440 Γ (0.025
2 )2 Γ 240 = 19.88
π
ππ=
π(π‘) β 36
600 β 36= πβ0.07Γ19.88
π(π‘) β 36
564= πβ1.3916
β΄ π(π‘) = 56 + πβ1.3916 + 36 = 176. 254ππΆ
πβ²(π)=0 = πβ²(0) = βπ΄π ππ = βπ΄π (ππ β πβ)
= 280 Γ 2π Γ 0.025 Γ 0.074(600 β 36) = 1835.65π€
πβ²(π)=4πππ = βπ΄π πππβπ΅π ΓπΉπ
14
= 1835.65 Γ πβ1.3916 = 456.5π€
Total heat transfer rate,
π(π‘) = βπ΄π ππ(1 β πβπ΅π ΓπΉπ)π
π΅π Γ πΉπ
π(π‘) = 1835.65(1 β πβ1.3916)240
1.3916= 237855.57 J
β 237.86 ππ
Example (4):
A piece of aluminum (π = 2705ππ/π3, π = 216π€/ππΎ, ππ = 896π/πππΎ) having a
mass of 4.78kg and initially at temperature of 290ππΆ is suddenly immersed in a fluid
at 15ππΆ.
The convection heat transfer coefficient is 54π€/π2πΎ . Taking the aluminum as a
sphere having the same mass as that given, estimate the time required to cool the
aluminum to 90ππΆ.
Find also the total heat transferred during this period. (Justify your use of the lumped
capacity method of analysis).
Solution:
A piece of aluminum
π = 2705ππ/π3; π = 216π€/ππΎ; ππ = 896π½/πππΎ; π = 4.78ππ
ππ = 290ππΆ;
πβ = 15ππΆ;
β = 24π€/π2πΎ;
Taking aluminum as a sphere.
Estimate π = ? π(π‘) = 90ππΆ ; π(π‘) =?
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅π ΓπΉπ
π΅π =β πΏ
π
15
The characteristic length, πΏ =π
π΄π =
4
3ππ3
4ππ2=
π
3
β΄ π΅π = β π
3π
π =π
π ; π =
π
π=
4.78
2705=
4
3ππ3
π = β4.78
2705Γ
3
4π
3
= 0.075π
β΄ π΅π =54 Γ 0.075
3 Γ 216= 0.00625
If π΅π βͺ 0.1 , then the system is assumed to be of lumped capacity.
Since π΅π = 0.00625 βͺ 0.1 , therefore the lumped capacity method of analysis is
used.
πΉπ =π
ππππΏ2β π =
216
2705 Γ 896 Γ (0.075
3 )2 β π
πΉπ = 0.1426 π
π
ππ=
90 β 15
290 β 15= πβ0.00625Γ0.1426 π
75
275= πβ8.9125Γ10β4 π
log75
275= β8.9125 Γ 10β4 π log π
β΄ π =log
75275
β8.9125 Γ 10β4 π log π= 1457.8 π
Total heat transfer rate, Q(t),
π(π‘) = βπ΄π ππ[1 β πβπ΅πΓπΉπ]π
π΅π Γ πΉπ
16
π(π‘) = 54 Γ 4π Γ 0.0752(290 β 15)[1 β πβ8.9125Γ10β4 Γ1457.8] Γ
1457.8
8.9125 Γ 10β4 Γ 1457.8= 856552 π½ = 856.6 ππ
β΄ π(π‘) = 856552 π½ = 856.6 ππ
17
Chapter Two
Time Constant and Response of Temperature Measuring
Instruments
2.1 Introduction:
Measurement of temperature by a thermocouple is an important application of
the lumped parameter analysis. The response of a thermocouple is defined as the time
required for the thermocouple to attain the source temperature.
It is evident from equation (1.4), that the larger the quantity βπ΄π
ππππ , the faster the
exponential term will approach zero or the more rapid will be the response of the
temperature measuring device. This can be accomplished either by increasing the
value of "h" or by decreasing the wire diameter, density and specific heat. Hence, a
very thin wire is recommended for use in thermocouples to ensure a rapid response
(especially when the thermocouples are employed for measuring transient
temperatures).
From equation (1.8);
π΅π Γ πΉπ
π=
βπ΄π
ππππ
ππππ
βπ΄π =
π
π΅π Γ πΉπ
The quantity ππππ
βπ΄π (which has units of time) is called time constant and is denoted by
the symbol πβ . Thus,
π
π΅π Γ πΉπ= πβ =
ππππ
βπ΄π =
π
πΌββ
π
π΄π (2.1)
{Since πΌ = π
πππ}
And,
18
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ = πβ(π/πβ) (2.2)
At π = πβ (one time constant), we have from equation (2.2),
π
ππ=
π(π‘) β πβ
ππ β πβ= πβ1 = 0.368 (2.3)
Thus, πβ is the time required for the temperature change to reach 36.8% of its final
value in response to a step change in temperature. In other words, temperature
difference would be reduced by 63.2%. The time required by a thermocouple to
reach its 63.2% of the value of initial temperature difference is called its sensitivity.
Depending upon the type of fluid used the response times for different sizes of
thermocouple wires usually vary between 0.04 to 2.5 seconds.
2.2 Solved Examples:
Example (1):
A thermocouple junction of spherical form is to be used to measure the temperature
of a gas stream.
β = 400π€/π2ππΆ; π(thermocouple junction) = 20π€/πππΆ; ππ = 400π½/ππππΆ;
and π = 8500ππ/π3;
Calculate the following:
(i) Junction diameter needed for the thermocouple to have thermal time constant of
one second.
(ii) Time required for the thermocouple junction to reach 198ππ if junction is initially
at 25ππΆ and is placed in gas stream which is at 200ππΆ .
Solution:
Given: β = 400π€/π2ππΆ; π(thermocouple junction) = 20π€/πππΆ;
ππ = 400π½/ππππΆ; π =8500ππ
π3.
(i) Junction diameter, d =?
πβ (thermal time constant) = 1 s
19
The time constant is given by:
πβ =ππππ
βπ΄π =
π Γ43
ππ3 Γ ππ
β Γ 4ππ2=
ππππ
3β
or 1 =8500 Γ π Γ 400
3 Γ 400
β΄ π = 3
8500= 3.53 Γ 10β4π = 0.353ππ
β΄ π = 2π = 2 Γ 0.353 = 0.706ππ
(ii) Time required for the thermocouple junction to reach 198ππΆ; π =?
Given: ππ = 25ππΆ; πβ = 200ππΆ; π(π‘) = 198ππΆ;
π΅π =β πΏπ
π
πΏπ of a sphere = π
3
β΄ π΅π =β(π/3)
π=
400 Γ (0.353 Γ 10β3/3)
20= 0.00235
As Bi is much less than 0.1, the lumped capacitance method can be used. Now,
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ = πβ(π/πβ)
πΉπ =π
ππππΏ2β π =
20
8500 Γ 400 Γ (0.353 Γ 10β3
3 )2 β π = 424.86 π
π΅π Γ πΉπ = 0.00235 Γ 424.86 π = 0.998π
β΄ π΅π Γ πΉπ =π
πβ= 0.998π
β΅ πβ = 1 , therefore, π = 0.998π
β΄π
ππ=
198 β 200
25 β 200= πβ0.998π
20
0.01143 = πβ0.998π
β0.998π ln π = ln 0.01143
β΄ π =ln 0.01143
β0.998 Γ 1= 4.48 π
Example (2):
A thermocouple junction is in the form of 8mm diameter sphere. Properties of
material are:
ππ = 420π½/ππππΆ; π = 8000ππ/π3; π = 40π€/πππΆ; β = 40π€/π2ππΆ;
This junction is initially at 40ππΆ and inserted in a stream of hot air at 300ππΆ . Find
the following:
(i) Time constant of the thermocouple.
(ii) The thermocouple is taken out from the hot air after 10 seconds and kept in still
air at 30ππΆ. Assuming the heat transfer coefficient in air ππ 10π€/π2ππΆ, find the
temperature attained by the junction 20 seconds after removal from hot air.
Solution:
Given: π =8
2= 4ππ = 0.004π; ππ =
420π½
ππππ; π =
8000ππ
π3; π = 40π€/πππΆ
β = 40π€/π2ππΆ (gas stream or hot air); β = 10π€/π2π
πΆ (still air)
(i) Time constant of the thermocouple, πβ =?
πβ =π
π΅π Γ πΉπ=
ππππ
βπ΄π =
π Γ43
ππ3 Γ ππ
β Γ 4ππ2=
ππππ
3β
β΄ πβ =8000 Γ 0.004 Γ 420
3 Γ 40= 112 π (when thermocouple is in gas stream)
(ii) The temperature attained by the junction, ; π(π‘) =?
Given: ππ = 40ππΆ; πβ = 300ππΆ; π = 10 π ;
The temperature variation with respect to time during heating (when dipped in gas
stream) is given by:
21
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ = πβ(π/πβ)
ππ π(π‘) β 300
40 β 300= πβ(π/πβ) = πβ(10/112) = 0.9146
β΄ π(π‘) = β260 Γ 0.9146 + 300 = 62.2ππΆ
The temperature variation with respect to time during cooling (when exposed to air)
is given by:
π(π‘) β πβ
ππ β πβ= πβ(π/πβ)
where πβ =ππππ
3β=
8000 Γ 0.004 Γ 420
3 Γ 10= 448 π
β΄ π(π‘) β 30
62.2 β 30= π(β20/448) = 0.9563
ππ π(π) = (62.2 β 30) Γ 0.9563 + 30 = 60.79ππΆ
Example (3):
A very thin glass walled 3mm diameter mercury thermometer is placed in a stream of
air, where heat transfer coefficient is 55π€/π2ππΆ, for measuring the unsteady
temperature of air. Consider cylindrical thermometer bulb to consist of mercury only
for which π = 8.8π€/πππΆ and πΌ = 0.0166π2/β. Calculate the time required for
the temperature change to reach half its final value.
Solution:
Given: π =3
2= 1.5ππ = 0.0015π; β = 55π€/π2π
πΆ; π = 8.8π€/πππΆ;
πΌ = 0.0166π2/β
The time constant is given by:
πβ =π
πΌββ
π
π΄π from equation (2.1)
β΄ πβ =π
πΌβΓ
ππ2πΏ
2πππΏ=
ππ
2πΌβ=
8.8 Γ 0.0015
2 Γ 0.0166 Γ 55= 0.0027229β = 26π
22
For temperature change to reach half its final value
π
ππ=
1
2= πβ(π/πβ)
ln1
2= ln πβπ/πβ
ln1
2= βπ/πβ ln π
βπ
πβ=
ln12
ln π= ln
1
2= β0.693
β΄π
πβ= 0.693
ππ π = πβ Γ 0.693 = 26 Γ 0.693 = 18.02 π
Note: Thus, one can expect thermometer to record the temperature trend accurately
only for unsteady temperature changes which are slower.
Example (4):
The temperature of an air stream flowing with a velocity of 3m/s is measured by a
copper β constantan thermocouple which may be approximately as a sphere of 2.5mm
in diameter. Initially the junction and air are at a temperature of 25ππΆ. The air
temperature suddenly changes to and is maintained at 215ππΆ.
(i) Determine the time required for the thermocouple to indicate a temperature of
165ππΆ. Also, determine the thermal time constant and the temperature indicated by
the thermocouple at that instant.
(ii) Discuss the stability of this thermocouple to measure unsteady state temperature
of a fluid when the temperature variation in the fluid has a time period of 3.6s.
The thermal junction properties are:
π = 8750ππ/π3; ππ = 380π½/ππππΆ; π(thermocouple) = 28π€/πππΆ; πππ
β = 145π€/π2ππΆ;
Solution:
23
Given: π =2.5
2= 1.25ππ = 0.00125π; ππ = 25ππΆ; πβ = 215ππΆ; π(π‘) = 165ππΆ
Time required to indicate temperature of 165ππΆ; π =? and πβ = ?;
Characteristic length,
πΏπ =π
π΄π =
43
ππ3
4ππ2=
π
3=
0.00125
3= 0.0004167π
Thermal diffusivity,
πΌ =π
πππ=
28
8750 Γ 380= 8.421 Γ 10β6π2/π
Fourier number,
πΉπ =π
ππππΏπ2
β π =πΌπ
πΏπ2
=8.421 Γ 10β6π
(0.0004167)2= 48.497 π
Biot number,
π΅π =βπΏπ
π=
145 Γ 0.0004167
28= 0.002158
As π΅π βͺ 0.1 , hence lumped capacitance method may be used for the solution of the
problem.
The temperature distribution is given by:
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
ππ 165 β 215
25 β 215= π(β0.002158Γ48.497π) = πβ0.1046π
0.263 = πβ0.1046π
β0.1046π ln π = ln 0.263
β΄ π =ln 0.263
β0.1046 Γ 1= 12.76 π
Thus, the thermocouple requires 12.76 s to indicate a temperature of 165ππΆ . The
actual time requirement will, however, be greater because of radiation from the probe
and conduction along the thermocouple lead wires.
24
The time constant (πβ) is defined as the time required to yield a value of unity for the
exponent term in the transient relation.
π΅π Γ πΉπ =π
πβ= 1
Or
0.002158 Γ 48.497 πβ = 1
Or
πβ = 9.55 π
At 9.55 s, the temperature indicated by the thermocouple is given by:
π(π‘) β πβ
ππ β πβ= πβ1
Or
π(π‘) β 215
25 β 215= πβ1
Or
π(π‘) = 215 + (25 β 215)πβ1 = 145ππ
(ii) As the thermal time constant is 9.55 s and time required to effect the temperature
variation is 3.6 s which is less than the thermal time constant, hence, the temperature
recovered by the thermocouple may not be reliable.
25
Chapter Three
Transient Heat Conduction in Solids with Finite Conduction
and Convective Resistances [π < π©π < πππ]
3.1 Introduction:
As shown in Fig. (3.1) below, consider the heating and cooling of a plane wall
having a thickness of 2L and extending to infinity in y and z directions.
Let us assume that the wall, initially, is at uniform temperature To and both the
surfaces (π₯ = Β±πΏ) are suddenly exposed to and maintained at the ambient (i.e.
surrounding) temperature πβ. The governing differential equation is:
π2π‘
ππ₯2=
1
πΌ
ππ‘
ππ (3.1)
The boundary conditions are:
(i) At π = 0 , π(π‘) = π0
(ii) At π = 0 ,ππ(π‘)
ππ₯= 0
(iii) At π₯ = Β±πΏ ; kAπT(t)
ππ₯= hA(T(t) β πβ)
(The conduction heat transfer equals convective heat transfer at the wall surface).
Fig. (3.1) Transient heat conduction in an infinite plane wall
The solutions obtained after rigorous mathematical analysis indicate that:
26
π(π‘) β πβ
ππ β πβ= π [
π₯
πΏ,βπ
π,πΌπ
π2] (3.2)
From equation (3.2), it is evident that when conduction resistance is not negligible,
the temperature history becomes a function of Biot numbers {βπ
π}, Fourier number
{πΌπ
π2 } and the dimensionless parameter {π₯
πΏ} which indicates the location of point within
the plate where temperature is to be obtained. The dimensionless parameter {π₯
πΏ} is
replaced by {π
π } in case of cylinders and spheres.
For the equation (3.2) graphical charts have been prepared in a variety of forms. In
the Figs. from (3.2) to (3.4) the Heisler charts are shown which depict the
dimensionless temperature [ππβπβ
ππβπβ] versus Fo (Fourier number) for various values of
(1
π΅π) for solids of different geometrical shapes such as plates, cylinders and spheres.
These charts provide the temperature history of the solid at its mid β plane (π₯ = 0)
and the temperatures at other locations are worked out by multiplying the mid β plane
temperature by correction factors read from charts given in figs. (3.5) to (3.7). The
following relationship is used:
π
ππ=
π(π‘) β πβ
ππ β πβ= [
ππ β πβ
ππ β πβ] Γ [
π(π‘) β πβ
ππ β πβ]
The values π΅π (Biot number) and πΉπ (Fourier number), as used in Heisler charts, are
evaluated on the basis of a characteristic parameter π which is the semi β thickness in
the case of plates and the surface radius in case of cylinders and spheres.
When both conduction and convection resistances are almost of equal importance the
Heister charts are extensively used to determine the temperature distribution.
3.2 Solved Examples:
Example (1):
A 60 mm thickness large steel plate (π = 42.6π€/πππΆ, πΌ = 0.043π2/β), initially at
440ππΆ is suddenly exposed on both sides to an environment with convective heat
transfer coefficient 235π€/π2ππΆ, and temperature 50ππΆ. Determine the center line
27
temperature, and temperature inside the plate 15ππ from the mid β plane after 4.3
minutes.
Solution:
Given: 2πΏ = 60ππ = 0.06π, π = 42.6π€/πππΆ, πΌ = 0.043π2/β, ππ = 440ππΆ,
β = 235π€/π2ππΆ, πβ = 50ππΆ, π = 4.3ππππ’π‘ππ .
Temperature at the mid β plane (centerline) of the plate ππ:
The characteristic length, πΏπ =60
2= 30ππ = 0.03π
Fourier number, πΉπ =πΌπ
πΏπ2 =
0.043Γ(4.3/60)
(0.03)2= 3.424
Biot number, π΅π =βπΏπ
π=
235Γ0.03
42.6= 0.165
At π΅π > 0.1, the internal temperature gradients are not small, therefore, internal
resistance cannot be neglected. Thus, the plate cannot be considered as a lumped
system. Further, as the π΅π < 100, Heisler charts can be used to find the solution of
the problem.
Corresponding to the following parametric values, from Heisler charts Fig. (3.2), we
have πΉπ = 3.424; 1
π΅π=
1
0.165= 6.06 and
π₯
πΏ= 0 (mid β plane).
ππ β πβ
ππ β πβ= 0.6 [from Heisler charts]
Substituting the values, we have
ππ β 50
440 β 50= 0.6
Or
ππ = 50 + 0.6(440 β 50) = 248ππΆ
Temperature inside the plate 15mm from the mid - plane, π(π‘) =? the distance 15mm
from the mid β plane implies that:
π₯
πΏ=
15
30= 0.5
Corresponding to π₯
πΏ= 0.5 and
1
π΅π= 6.06, from Fig. (3.5), we have:
28
π(π‘) β πβ
ππ β πβ= 0.97
Substituting the values, we get:
π(π‘) β 50
284 β 50= 0.97
Or
π(π‘) = 50 + 0.97(284 β 50) = 276.98ππΆ
Example (2):
A 6 mm thick stainless steel plate (π = 7800ππ/π3, ππ = 460π½/ππππΆ, π =
55π€/πππΆ) is used to form the nose section of a missile. It is held initially at a
uniform temperature of 30ππΆ. When the missile enters the denser layers of the
atmosphere at a very high velocity the effective temperature of air surrounding the
nose region attains 2150ππΆ; the surface convective heat transfer coefficient is
estimated 3395π€/π2ππΆ. If the maximum metal temperature is not to exceed
1100ππΆ, determine:
(i) Maximum permissible time in these surroundings.
(ii) Inside surface temperature under these conditions.
Solution:
Given: 2πΏ = 6ππ = 0.006π, π = 55π€/πππΆ, ππ = 460π½/πππ πΆ, ππ = 30ππΆ,
π = 7800ππ/π3, πβ = 2150ππΆ, π(π‘) = 1100ππΆ
(i) Maximum permissible time, π = ?
Characteristic length, πΏπ =0.006
2= 0.003π
Biot number, π΅π =βπΏ
π=
3395Γ0.003
55= 0.185
As π΅π > 0.1, therefore, lumped analysis cannot be applied in this case. Further, as
π΅π < 100, Heisler charts can be used to obtain the solution of the problem.
Corresponding to 1
π΅π= 5.4 and
π₯
πΏ= 1 (outside surface of nose section, from Fig.
(3.5), we have),
29
π(π‘) β πβ
ππ β πβ= 0.93
Also,
π
ππ=
π(π‘) β Tβ
ππ β πβ= [
ππ β πβ
ππ β πβ] Γ [
π(π‘) β πβ
ππ β πβ]
Or
1100 β 2150
30 β 2150= [
ππ β πβ
ππ β πβ] Γ 0.93
Or
ππ β πβ
ππ β πβ=
1
0.93[1100 β 2150
30 β 2150] = 0.495
Now, from Fig. (3.2), corresponding to the above dimensionless temperature and
1
π΅π= 5, we got the value of Fourier number, πΉπ = 4.4
β΄πΌπ
πΏπ2
= 4.4
Or
[π
πππ] [
π
πΏπ2
] = 4.4
Or
[55
7800 Γ 460] [
π
0.0032] = 4.4
Or
π =4.4 Γ 0.0032 Γ 7800 Γ 460
55= 2.58π
(ii) Inside surface temperature, ππ =?
The temperature ππ at the inside surface (π₯ = 0) is given by:
ππ β πβ
ππ β πβ= 0.495
Or
ππ β 2150
30 β 2150= 0.495
30
Or
ππ = 2150 + 0.495(30 β 2150) = 1100.6ππΆ
Example (3):
Along cylindrical bar (π = 17.4π€/ππ πΆ , πΌ = 0.019π2/β) of radius 80ππ comes
out of an oven at 830π πΆ throughout and is cooled by quenching it in a large bath of
40π πΆ coolant. The surface coefficient of heat transferred between the bar surface and
the coolant is 180π€/π2 ππΆ . Determine:
(i) The time taken by the shaft center to reach 120π πΆ .
(ii) The surface temperature of the shaft when its center temperature is 120π πΆ. Also,
calculate the temperature gradient at outside surface at the same instant of time.
Solution:
Given: π = 80ππ = 0.08π, ππ = 830ππΆ, πβ = 40ππΆ, β = 180π€/π2 ππΆ,
π(π‘) = 120π πΆ, π = 17.4π€/ππ πΆ, πΌ = 0.019 π2/β.
(i) The time taken by the shaft center to reach 120ππΆ, π = ?
Characteristic length, πΏπ =ππ 2πΏ
2ππ πΏ=
π
2=
0.08
2= 0.04π
Biot number, π΅π =βπΏπ
π=
180Γ0.04
17.4= 0.413
As π΅π > 0.1, therefore, lumped analysis cannot be applied in this case. Further, as
π΅π < 100, Heisler charts can be used to obtain the solution of the problem.
The parametric values for the cylindrical bar are:
1
π΅π=
1
0.413= 2.42
π(π‘) β πβ
ππ β πβ=
120 β 40
830 β 40= 0.1
At the center of the bar, π
π = 0
Corresponding to the above values, from the chart for an infinite cylinder Fig. (3.3),
we read the Fourier number πΉπ = 3.2 .
β΄ πΌπ
(πΏπ)2= 3.2 ππ
0.019 Γ π
0.042= 3.2
31
Or
π =3.2 Γ 0.042
0.019= 0.2695β ππ 970.2π
(ii) Temperature at the surface, π(π‘) ππ ππ = ?
Corresponding to π
π = 1;
1
π΅π= 2.42 , from the chart Fig. (3.6) for an infinite
cylinder, we read,
π(π‘) β πβ
ππ β πβ= 0.83
Or
π(π‘) β 40
120 β 40= 0.83
Or
π(π‘) β 40 = 0.83(120 β 40)
Or
π(π‘) ππ ππ = 40 + 0.83(120 β 40) = 106.4ππΆ
Temperature gradient at the outer surface, πππ
ππ=?
πππ
ππ at the outside surface is determined by the boundary condition π = π , at which,
rate of energy conducted to the fluid β solid surface interface from within the solid =
rate at which energy is convected away into the fluid.
ππ΄π
ππ
ππ= βπ΄π (ππ β πβ)
Or
πππ
ππ= β(ππ β πβ)
Or
ππ
ππ=
β
π(ππ β πβ)
Or
πππ
ππ=
180
17.4(106.4 β 40) = 686.89 ππΆ
32
Example (4):
A 120ππ diameter apple π = 990ππ/π3, ππ = 4170π½/πππ πΆ, π = 0.58π€/πππΆ),
approximately spherical in shape is taken from a 25ππΆ environment and placed in a
refrigerator where temperature is 6ππΆ and the average convective heat transfer
coefficient over the apple surface is 12.8π€/π2ππΆ. Determine the temperature at the
center of the apple after a period of 2 hours.
Solution:
Given: π = 120/2 = 60ππ = 0.06π, π = 990ππ/π3, ππ = 4170π½/ππππΆ,
π = 0.58π€/πππΆ, ππ = 25ππΆ, πβ = 6ππΆ, β = 18.8π€/π2ππΆ, π = 2βππ’ππ = 7200π
The characteristic length, πΏπ =4
3ππ 3
4ππ 2=
π
3=
0.06
3= 0.02π
Biot number, π΅π =βπΏπ
π=
12.8Γ0.02
0.58= 0.441 ,
Since π΅π > 0.1, a lumped capacitance approach is appropriate.
Further, as π΅π < 100, Heisler charts can be used to obtain the solution of the
problem.
The parametric values for the spherical apple are:
1
π΅π=
1
0.441= 2.267
πΉπ =πΌπ
(πΏπ)2= [
π
πππ]
π
πΏπ2
= [0.58
990 Γ 4170] Γ [
7200
0.022] = 0.281
π
π = 0 (mid β plane or center of the apple)
Corresponding to the above values, from the chart for a sphere Fig. (3.7), we read
ππ β πβ
ππ β πβ= 0.75
Or
ππ β 6
25 β 6= 0.75
Or
ππ = 6 + 0.75(25 β 6) = 20.25 ππΆ
33
Fig
. (3
.2)
Hei
sler
ch
art
fo
r te
mp
era
ture
his
tory
at
the
cen
ter
of
a p
late
of
thic
kn
ess
2L
or
(x/L
) =
0
36
Fig. (3.5) Heisler position β correction factor chart for temperature history in
plate
Fig. (3.6) Heisler position β correction factor chart for temperature history in
cylinder
38
Chapter Four
Transient Heat conduction in semi β infinite solids
[π― ππ π©π β β] 4.1 Introduction:
A solid which extends itself infinitely in all directions of space is termed as an
infinite solid. If an infinite solid is split in the middle by a plane, each half is known
as semi β infinite solid. In a semi β infinite body, at any instant of time, there is
always a point where the effect of heating (or cooling) at one of its boundaries is not
felt at all. At the point the temperature remains unaltered. The transient temperature
change in a plane of infinitely thick wall is similar to that of a semi β infinite body
until enough time has passed for the surface temperature effect to penetrate through
it.
As shown in Fig. (4.1) below, consider a semi β infinite plate, a plate bounded by a
plane π₯ = 0 and extending to infinity in the (+π£π) x β direction. The entire body is
initially at uniform temperature ππ including the surface at π₯ = 0. The surface
temperature at π₯ = 0 is suddenly raised to πβ for all times greater than π = 0 . The
governing equation is:
π2π‘
ππ₯2=
1
πΌ ππ‘
ππ (4.1)
Fig. (4.1) Transition heat flow in a semi β infinite plate
39
The boundary conditions are:
(i) π(π₯, 0) = ππ ;
(ii) π(0, π) = πβ πππ π > 0 ;
(iii) π(β, π) = ππ πππ π > 0 ;
The solution of the above differential equation, with these boundary conditions, for
temperature distribution at any time π at a plane parallel to and at a distance π₯ from
the surface is given by:
π(π₯, π) β πβ
ππ β πβ= erf (π§) = πππ [
π₯
2βπΌπ] (4.2)
Where π§ =π₯
2βπΌπ is known as Gaussian error function and is defined by:
πππ [π₯
2βπΌπ] = erf(π§) =
2
βπβ« πβπ2
ππ (4.3)π§
0
With erf(0) = 0, erf (β) = 1.
Table (4.1) shows a few representative values of erf(π§). Suitable values of error
functions may be obtained from Fig. (4.2) below.
Fig. (4.2) Gauss's error integral
40
Table (4.1) The error function
erf(π§) =2
βπβ« πβπ2
ππ where π§ =π₯
2βπΌπ
π§
0
π§ erf (π§) π§ erf (π§)
0.00 0.0000 0.32 0.3491
0.02 0.0225 0.34 0.3694
0.04 0.0451 0.36 0.3893
0.06 0.0676 0.38 0.4090
0.08 0.0901 0.40 0.4284
0.10 0.1125 0.42 0.4475
0.12 0.1348 0.44 0.4662
0.14 0.1569 0.46 0.4847
0.16 0.1709 0.48 0.5027
0.18 0.2009 0.50 0.5205
0.20 0.2227 0.55 0.5633
0.22 0.2443 0.60 0.6039
0.024 0.2657 0.65 0.6420
0.26 0.2869 0.70 0.6778
0.28 0.3079 0.75 0.7112
0.30 0.3286 0.80 0.7421
0.85 0.7707 1.65 0.9800
0.90 0.7970 1.70 0.9883
0.95 0.8270 1.75 0.9864
1.00 0.8427 1.80 0.9891
1.05 0.8614 1.85 0.9909
1.10 0.8802 1.90 0.9928
1.15 0.8952 1.95 0.9940
1.20 0.9103 2.00 0.9953
1.25 0.9221 2.10 0.9967
1.30 0.9340 2.20 0.9981
1.35 0.9431 2.30 0.9987
1.40 0.9523 2.40 0.9993
1.45 0.9592 2.50 0.9995
1.50 0.9661 2.60 0.9998
1.55 0.9712 2.80 0.9999
1.60 0.9763 3.00 1.0000
By insertion of definition of error function in equation (4.2), we get
π(π₯, π) = πβ + (ππ β πβ)2
βπβ« πβπ2
ππ π§
0
On differentiating the above equation, we obtain
ππ
ππ₯=
ππ β πβ
βπ πΌ π π[βπ₯2/(4 πΌ π)]
41
The instantaneous heat flow rate at a given x β location within the semi β infinite
body at a specified time is given by:
ππππ π‘πππ‘πππππ’π = βππ΄(ππ β πβ)π
[βπ₯2
4 πΌ π]
βπ πΌ π (4.4)
By substituting the gradient [ππ
ππ₯] in Fourier's law.
The heat flow rate at the surface (π₯ = 0) is given by:
ππ π’πππππ =βππ΄(ππ β πβ)
βπ πΌ π (4.5)
The total heat flow rate,
π(π‘) =βππ΄(ππ β πβ)
βπ πΌ β«
1
βπππ = βππ΄(ππ β πβ)2β
π
ππΌ
π
0
Or
π(π‘) = β1.13ππ΄(ππ β πβ)βπ
πΌ (4.6)
The general criterion for the infinite solution to apply to a body of finite thickness
(slab) subjected to one dimensional heat transfer is:
πΏ
2βπΌ π β₯ 0.5
Where, L = thickness of the body.
The temperature at the center of cylinder or sphere of radius R, under similar
conditions of heating or cooling, is given as follows:
π(π‘) β πβ
ππ β πβ= πππ [
πΌπ
π 2] (4.7)
For the cylindrical and spherical surfaces the values of function πππ [πΌπ
π 2] can be
obtained from Fig. (4.3) which is shown below.
42
Fig. (4.3) Error integral for cylinders and spheres
4.2 Penetration Depth and Penetration Time:
Penetration depth refers to the location of a point where the temperature change
is within 1 percent of the change in the surface temperature.
π. π. π(π‘) β πβ
ππ β πβ= 0.9
This corresponds to π₯
2βπΌπ= 1.8 , from the table for Gaussian error integral.
Thus, the depth (π) to which the temperature perturbation at the surface has
penetrated,
π = 3.6 βπΌ π
Penetration time is the time ππ taken for a surface penetration to be felt at that depth
in the range of 1 percent. It is given by:
π
2 βπΌ ππ
= 1.8
Or
43
ππ =π2
13 πΌ (4.8)
4.3 Solved Examples:
Example (1):
A steel ingot (large in size) heated uniformly to 745π πΆ is hardened by quenching it
in an oil path maintained at 20π πΆ. Determine the length of time required for the
temperature to reach 595π πΆ at a depth of 12ππ. The ingot may be approximated as
a flat plate. For steel ingot take πΌ(thermal diffusivity) = 1.2 Γ 10β5π2/π
Solution:
Given: ππ = 745ππ, πβ = 20ππ, π(π‘) = 595ππ, π₯ = 12ππ = 0.012π,
πΌ = 1.2 Γ 10β5π2/π , time required, π =?
The temperature distribution at any time π at a plane parallel to and at a distance π₯
from the surface is given by:
π(π‘) β πβ
ππ β πβ= πππ [
π₯
2 βπΌ π] (4.2)
Or
595 β 20
745 β 20= 0.79 = πππ [
π₯
2 βπΌ π]
Or
β΄ π₯
2 βπΌ π= 0.9 from Table (4.1) or Fig. (4.3)
Or
π₯2
4 πΌ π= 0.81
Or
π =π₯2
4 πΌ Γ 0.81=
0.0122
4 Γ 1.2 Γ 10β5 Γ 0.81= 3.7π
Example (2):
It is proposed to bury water pipes underground in wet soil which is initially at 5.4π πΆ.
The temperature of the surface of soil suddenly drops to β6π πΆ and remains at this
44
value for 9.5 hours. Determine the maximum depth at which the pipes be laid if the
surrounding soil temperature is to remain above 0π πΆ (without water getting frozen).
Assume the soil as semi β infinite solid.
For wet soil take πΌ(thermal diffusivity) = 2.75 Γ 10β3π2/β
Solution:
Given: ππ = 5.4ππΆ, πβ = β6ππ, π(π‘) = 0ππΆ, πΌ = 2.75 Γ 10β3π2/π , maximum
depth π₯ =?
The temperature, at critical depth, will just reach after 9.5 hours,
Now,
π(π‘) β πβ
ππ β πβ= πππ [
π₯
2 βπΌ π] (4.2)
Or
0 β (β6)
5.4 β (β6)= 0.526 = πππ [
π₯
β2 πΌ π]
Or
π₯
2 βπΌ πβ 0.5 from Table (4.1)or Fig. (4.3)
Or
π₯ = 0.5 Γ 2 βπΌ π
Or
π₯ = 0.5 Γ 2 β2.75 Γ 10β3 Γ 9.5 = 0.162π
Example (3):
A 60ππ thick mild steel plate (πΌ = 1.22 Γ 10β5π2/π ) is initially at a temperature
of 30π πΆ. It is suddenly exposed on one side to a fluid which causes the surface
temperature to increase to and remain at 110π πΆ . Determine:
(i) The maximum time that the slab be treated as a semi β infinite body;
(ii) The temperature at the center of the slab 1.5 minutes after the change in surface
temperature.
45
Solution:
Given: πΏ = 60ππ = 0.06π, πΌ = 1.22 Γ 10β5π2/π , ππ = 30ππΆ, πβ = 110ππΆ,
π = 1.5 ππππ’π‘ππ = 90 π
(i) The maximum time that the slab be treated as a semi β infinite body, (ππππ₯ = ).
The general criterion for the infinite solution to apply to a body of finite thickness
subjected to one β dimensional heat transfer is:
πΏ
2 βπΌ πβ₯ 0.5 (where L = thickness of the body)
Or
πΏ
2 βπΌ ππππ₯
= 0.5 or πΏ2
4 πΌ ππππ₯= 0.25
Or
ππππ₯ =πΏ2
4 πΌ Γ 0.25=
0.062
4 Γ 1.22 Γ 10β5 Γ 0.25= 295.1 π
(ii) The temperature at the center of the slab, π(π‘) =?
At the center of the slab, π₯ = 0.03π ; π = 90 π
π(π‘) β πβ
ππ β πβ= πππ [
π₯
2 βπΌ π]
Or
π(π‘) = πβ + πππ [π₯
2 βπΌ π] (ππ β πβ)
Where:
πππ [π₯
2 βπΌ π] = πππ [
0.03
2 β1.22 Γ 10β5 Γ 90] = erf(0.453)
β 0.47 [from Table (4.1)]
π(π‘) = ππ = 110 + 0.47(30 β 110) = 72.4ππΆ
Example (4):
The initial uniform temperature of a thick concrete wall (πΌ = 1.6 Γ 10β3π2/β, π =
0.9π€/πππΆ) of a jet engine test cell is 25ππΆ. The surface temperature of the wall
46
suddenly rises to 340ππΆ when the combination of exhaust gases from the turbo jet β¦
spray of cooling water occurs. Determine:
(i) The temperature at a point 80mm from the surface after 8 hours.
(ii) The instantaneous heat flow rate at the specified plane and at the surface itself at
the instant mentioned at (i).
Use the solution for semi β infinite solid.
Solution:
Given: ππ = 25ππΆ, πβ = 340ππΆ, πΌ = 1.6 Γ 10β3π2/β, π = 0.94π€/πππΆ, π = 8β,
π₯ = 80ππ = 0.08π
(i) The temperature at a point 0.08m from the surface; π(π‘) =?
π(π‘) β πβ
ππ β πβ= πππ [
π₯
2 βπΌ π]
Or
π(π‘) = πβ + πππ [π₯
2 βπΌ π] (ππ β πβ)
Where
πππ [π₯
2 βπΌ π] = πππ [
0.03
2 β1.6 Γ 10β3 Γ 8] = erf(0.353) β 0.37
β΄ π(π‘) = 340 + 0.37(25 β 340) = 223.45ππΆ
(ii) The instantaneous heat flow rate, ππππ π‘πππ‘πππππ’π at the specified plane =?
ππ = βππ΄(ππ β πβ)π
[βπ₯2
4 πΌ π]
βπ πΌ π from equation (4.4)
ππ = β0.94 Γ 1 Γ (25 β 340)π[β0.082/(4Γ1.6Γ10β3Γ8)]
βπ Γ 1.6 Γ 10β3 Γ 8
= β296.1 Γ0.8825
0.2005= β1303.28π€/π2 of wall area
The negative sign shows the heat lost from the wall.
Heat flow rate at the surface itself, ππ π’πππππ =?
47
ππ π’πππππ ππ ππ = βππ΄(ππ β πβ)
βπ πΌ π from equation(4.5)
= β0.94 Γ 1 Γ (25 β 340)
βπ Γ 1.6 Γ 10β3 Γ 8 = (β)1476.6π€ per π2 of wall area
Example (5):
The initial uniform temperature of a large mass of material (πΌ = 0.42π2/β) is
120ππΆ. The surface is suddenly exposed to and held permanently at 6ππΆ. Calculate
the time required for the temperature gradient at the surface to reach 400ππΆ/π.
Solution:
Given: ππ = 120ππΆ, πβ = 6ππΆ, πΌ = 0.42π2/β,
[π π
π π₯]
π₯=0 (temperature gradient at the surface) = 400ππΆ/π
Time required, π =?
Heat flow rate at the surface (π₯ = 0) is given by:
ππ π’πππππ = βππ΄(ππ β πβ)
βπ πΌ π from equation (4.5)
Or
βππ΄ [π π
π π₯]
π₯=0 = β
ππ΄(ππ β πβ)
βπ πΌ π
Or
[π π
π π₯]
π₯=0 =
ππ β πβ
βπ πΌ π
substituting the values above, we obtain:
400 =(120 β 6)
βπ Γ 0.42 Γ π
Or
π Γ 0.42π = [120 β 6
400]
2
= 0.0812
Or
48
π =0.0812
π Γ 0.42= 0.0615β = 221.4 π
Example (6):
A motor car of mass 1600kg travelling at 90km/h, is brought to reset within a period
of 9 seconds when the brakes are applied. The braking system consists of 4 brakes
with each brake band of 360 cm2 area, these press against steel drums of equivalent
area. The brake lining and the drum surface (π = 54π€/πππΆ, πΌ = 1.25 Γ 10β5π2/π )
are at the same temperature and the heat generated during the stoppage action
dissipates by flowing across drums. The drum surface is treated as semi β infinite
plane, calculate the maximum temperature rise.
Solution:
Given: π = 1600ππ, π£(velocity) = 90ππ/β, π = 9π , π΄(Area of 4 brake bands)
= 4 Γ 360 Γ 10β4π2 ππ 0.144π2, π = 54π€/πππΆ, πΌ = 1.25 Γ 10β5π2/π .
Maximum temperature rise, πβ β ππ =?
When the car comes to rest (after applying brakes), its kinetic energy is converted
into heat energy which is dissipated through the drums.
Kinetic energy of the moving car = 1
2ππ£2
=1
2Γ 1600 Γ [
90 Γ 1000
60 Γ 60]
2
= 5 Γ 105J in 9 seconds
β΄ Heat flow rate = 5 Γ 105
9= 0.555 Γ 105J /s ππ π€
This value equals the instantaneous heat flow rate at the surface (π₯ = 0), which is
given by:
(ππ)π π’πππππ = βππ΄(ππ β πβ)
βπ πΌ π= 0.555 Γ 105 from equation (4.5)
Or
β54 Γ 0.144(ππ β πβ)
βπ Γ 1.25 Γ 10β5 Γ 9= 0.555 Γ 105
49
Or
β(ππ β πβ) =0.555 Γ 105 Γ βπ Γ 1.25 Γ 10β5 Γ 9
54 Γ 0.144= 134.3
Or
ππ β πβ = 134.3ππΆ
Hence, maximum temperature rise = 134.3ππΆ
Example (7):
A copper cylinder (πΌ = 1.12 Γ 10β4π2/π ), 600ππ in diameter and 750ππ in
length, is initially at a uniform temperature of 20ππΆ. When the cylinder is exposed to
hot flue gases, its surface temperature suddenly increases to 480ππΆ. Calculate:
(i) The temperature at the center of cylinder 3 minutes after the operation of change
in surface temperature;
(ii) Time required to attain a temperature of 350ππΆ.
Assume the cylinder as semi β infinite solid.
Solution:
Given: π =600
2= 300ππ or 0.3π, πΌ = 1.12 Γ 10β4π2/π , ππ = 20ππΆ,
πβ = 480ππΆ, π(π‘) = 350ππΆ, π = 3 Γ 60 = 180 π
(i) The temperature at the center of the cylinder, π(π‘) or ππ = ?
The temperature distribution at the center of the cylinder is expressed as:
π(π‘) β πβ
ππ β πβ= πππ [
πΌ π
π 2] from equation (4.7)
Where:
πππ [πΌ π
π 2] = πππ [
1.12 Γ 10β4 Γ 180
0.32] = πππ(0.224) β 0.32 [from Fig. (4.3)]
Substituting the values, we obtain:
π(π‘) β 480
20 β 480= 0.32
Or
π(π‘) = 480 + 0.32(20 β 480) = 332.8ππΆ
50
(ii) Time required to attain a temperature of 350ππΆ, π =?
350 β 480
20 β 480= πππ [
πΌ π
π 2]
0.2826 = πππ [πΌ π
π 2]
β΄ πΌ π
π 2β 0.23
Or
π =0.23 Γ π 2
πΌ=
0.23 Γ 0.32
1.12 Γ 10β4= 184.8 π
51
Chapter Five
Systems with Periodic Variation of Surface Temperature
5.1 Introduction:
The periodic type of heat flow occurs in cyclic generators, in reciprocating
internal combustion engines and in the earth as the result of daily cycle of the sun.
These periodic changes, in general, are not simply sinusoidal but rather complex.
However, these complex changes can be approximated by a number of sinusoidal
components.
Let us consider a thick plane wall (one dimensional case) whose surface
temperature alters according to a sine function as shown in Fig. (5.1) below. The
surface temperature oscillates about the mean temperature level π‘π according to the
following relation:
ππ ,π = ππ ,π sin (2πππ)
Where,
ππ ,π = excess over the mean temperature (= π‘π ,π β π‘π);
ππ ,π = Amplitude of temperature excess, i.e., the maximum temperature excess at the
surface;
π = Frequency of temperature wave.
The temperature excess at any depth π₯ and time π can be expressed by the following
relation:
52
Fig. (5.1) Temperature curves for periodic variation of surface temperature
ππ₯,π = ππ ,π exp[βπ₯βππ/πΌ]π ππ [2πππ β π₯βππ
πΌ] (5.1)
The temperature excess, at the surface (π₯ = 0), becomes zero at π = 0. But at any
depth, π₯ > 0, a time [[π₯
2] [
1
βπΌ π π]] would elapse before the temperature excess ππ₯,π
becomes zero. The time interval between the two instant is called the time lag.
The time lag βπ =π₯
2β
1
πΌ π π (5.2)
At depth π₯, the temperature amplitude (ππ₯,π) is given by:
ππ₯,π = ππ ,π exp [βπ₯βπ π
πΌ] (5.3)
The above relations indicate the following facts:
1. At any depth, π₯ > 0, the amplitude (maximum value) occurs late and is smaller
than that at the surface (π₯ = 0).
2. The amplitude of temperature oscillation decreases with increasing depth.
(Therefore, the amplitude becomes negligibly small at a particular depth inside the
53
solid and consequently a solid thicker than this particular depth is not of any
importance as far as variation in temperature is concerned).
3. With increasing value of frequency, time lag and the amplitude reduce.
4. Increase in diffusivity πΌ decreases the time lag but keeps the amplitude large.
5. The amplitude of temperature depends upon depth π₯ as well as the factor βπ
πΌ .
Thus, if βπ
πΌ is large, equation (5.3) holds good for thin solid rods also.
5.2 Solved Examples:
Example (1):
During the periodic heating and cooling of a thick brick wall, the wall temperature
varies sinusoidally. The surface temperature ranges from 30ππΆ to 80ππΆ during a
period of 24 hours. Determine the time lag of the temperature wave corresponding to
a point located at 300mm from the wall surface.
The properties of the wall material are:
π = 1610ππ/π3, π = 0.65π€/πππΆ; ππ = 440π½/ππππΆ
Solution:
Given: π₯ = 300ππ = 0.3π, π = 1610ππ/π3, π = 0.65π€/πππΆ;
ππ = 440π½/ππππΆ, π =1
24= 0.04167/β
Time lag β π =?
β π =π₯
2β
1
πΌ π π from equation (5.2)
Where:
πΌ =π
πππ=
0.65
1610 Γ 440= 9.176 Γ 10β7 π2/π or 0.0033π2/β
β΄ β π =0.3
2Γ β
1
0.0033 Γ π Γ 0.04167= 7.2 β
54
Example (2):
A single cylinder (πΌ = 0.044π2/β for cylinder material) two β stroke I.C. engine
operates at 1400 rev/min. Calculate the depth where the temperature wave due to
variation of cylinder temperature is damped to 2% of its surface value.
Solution:
Given: πΌ = 0.044π2/β, π = 1400 Γ 60 = 84000/β
The amplitude of temperature excess, at any depth π₯, is given by:
ππ₯,π = ππ ,π πβπ₯β
π ππΌ from equation (5.3)
Or
ππ₯,π
ππ ,π= π
βπ₯βπ ππΌ
Or
2
100= π
βπ₯βπΓ840000.044 = πβ2449π₯
πΌπ 0.02 = β2449 π₯ πΌππ
π₯ =πΌπ 0.02
β2449 Γ 1= 1.597 Γ 10β3π or 1.597ππ
55
Chapter Six
Transient Conduction with Given Temperature Distribution
6.1 Introduction:
The temperature distribution at some instant of time, in some situations, is
known for the one β dimensional transient heat conduction through a solid.
The known temperature distribution may be expressed in the form of polynomial
π‘ = π β ππ₯ + ππ₯2 + ππ₯3 β ππ₯4 Where π, π, π, π and π are the known coefficients.
By using such distribution, the one β dimensional transient heat conduction problem
can be solved.
6.2 Solved Examples:
Example (1):
The temperature distribution across a large concrete slab 500ππ thick heated from
one side as measured by thermocouples approximates to the following relation,
π‘ = 120 β 100π₯ + 24π₯2 + 40π₯3 β 30π₯4
Where t is in ππΆ and π₯ is in π. Considering an area of 4π2, Calculate:
(i) The heat entering and leaving the slab in unit time;
(ii) The heat energy stored in unit time;
(iii) The rate of temperature change at both sides of the slab;
(iv) The point where the rate of heating or cooling is maximum.
The properties of concrete are as follows:
π = 1.2 π€/πππΆ, πΌ = 1.77 Γ 10β3π2/β
Solution:
Given: π΄ = 4π2, π₯ = 500ππ = 0.5π, π = 1.22π€/πππΆ, πΌ = 1.77 Γ 10β3π2/β
π‘ = 120 β 100π₯ + 24π₯2 + 40π₯3 β 30π₯4 (Temperature distribution polynomial)
ππ‘
ππ₯= β100 + 48π₯ + 120π₯2 β 120π₯3
π2π‘
ππ₯2= 48 + 240π₯ β 360π₯2
56
(i) The heat entering and leaving the slab in unit time: ππ =? ππ =?
Heat leaving the slab,
πππ = βππ΄ [ππ‘
ππ₯]
π₯=0= (β1.2 Γ 5)(β100) = 600π€
Heat leaving the slab,
πππ’π‘ = βππ΄ [ππ‘
ππ₯]
π₯=0.5= (β1.2 Γ 5)(β100 + 48 Γ 0.5 + 120 Γ 0.52 β 120 Γ 0.52)
= 0.6(β100 + 24 + 30 β 15) = 366π€
(ii) The heat energy stored in unit time:
rate of heat storage = πππ β πππ’π‘ = 600 β 366 = 234π€
(iii) The rate of temperature change at both sides of the slab: [ππ‘
ππ]
π₯=0 and [
ππ‘
ππ]
π₯=0.5=?
ππ‘
ππ= πΌ
π2π‘
ππ₯2= πΌ(48 + 240π₯ β 360π₯2)
β΄ [ππ‘
ππ]
π₯=0= 1.77 Γ 10β3(48) = 0.08496 ππΆ/β
and, [ππ‘
ππ]
π₯=0.5= 1.77 Γ 10β3(48 + 240 Γ 0.5 β 360 Γ 0.52) = 1.3806 ππ/β
(iv) The point where the rate of heating or cooling is maximum, π₯:
π
ππ₯[ππ‘
ππ] = 0
Or
π
ππ₯[πΌ
π2π‘
ππ₯2] = 0
Or
π3π‘
ππ₯3= 0
Or
58
Chapter Seven
Additional Solved Examples in Lumped Capacitance System
7.1 Example (1): Determination of Temperature and Rate of Cooling
of a Steel Ball
A steel ball 100mm in diameter and initially at 900ππΆ is placed in air at 30ππΆ, find:
(i) Temperature of the ball after 30 seconds.
(ii) The rate of cooling (ππΆ/πππ.) after 30 seconds.
Take: β = 20π€/π2ππΆ; π(steel) = 40π€/πππΆ; π(steel) = 7800ππ/π3;
ππ(steel) = 460π½/ππππΆ
Solution:
Given: π =100
2= 50ππ or 0.05π; ππ = 900ππΆ; πβ = 30ππΆ, β = 20π€/π2π
πΆ;
π(steel) = 40π€/πππΆ; π(steel) = 7800ππ/π3; ππ(steel) = 460π½/ππππΆ;
π = 30π
(i) Temperature of the ball after 30 seconds: π(π‘) =?
Characteristic length,
πΏπ =π
π΄π =
43
ππ 3
4ππ 2=
π
3=
0.05
3= 0.01667π
Biot number,
π΅π =βπΏπ
π=
20 Γ 0.01667
40= 0.008335
Since, π΅π is less than 0.1, hence lumped capacitance method (Newtonian heating or
cooling) may be applied for the solution of the problem.
The time versus temperature distribution is given by equation (1.4):
π
ππ=
π(π‘) β πβ
ππ β πβ= π
ββπ΄π ππππ (1)
Now,
59
βπ΄π
ππππβ π [
β
πππ] [
π΄π
π] π = [
20
7800 Γ 460] [
1
0.01667] (30) = 0.01
β΄ π(π‘) β 30
900 β 30= πβ0.01 = 0.99
Or
π(π‘) = 30 + 0.99(900 β 30) = 891.3ππΆ
(ii) The rate of cooling (ππΆ/min) after 30 seconds: ππ‘
ππ=?
The rate of cooling means we have to find out ππ‘
ππ at the required time. Now,
differentiating equation (1), we get:
1
ππ β πβΓ
ππ‘
ππ= β [
βπ΄π
ππ£ππ] π
ββπ΄π ππππ
π
Now, substituting the proper values in the above equation, we have:
1
(900 β 30)β
ππ‘
ππ= β [
20
7800 Γ 460Γ
1
0.01667] Γ 0.99 = β3.31 Γ 10β4
β΄ ππ‘
ππ= (900 β 30)(β3.31 Γ 10β4) = β0.288ππΆ/π
ππ ππ‘
ππ= β0.288 Γ 60 = β17.28ππ/πππ
7.2 Example (2): Calculation of the Time Required to Cool a Thin
Copper Plate
A thin copper plate 20ππ thick is initially at 150ππΆ. One surface is in contact with
water at 30ππ (βπ€ = 100π€/π2ππΆ) and the other surface is exposed to air at 30ππΆ
(βπ = 20π€/π2ππΆ). Determine the time required to cool the plate to 90ππΆ.
Take the following properties of the copper:
π = 8800ππ/π3; ππ = 400π½/ππππΆ πππ π = 360π€/πππΆ
The plate is shown in Fig. (7.1) below:
Solution:
Given: πΏ = 20ππ or 0.02π; ππ = 150ππΆ; πβ = 30ππΆ, βπ€ = 100π€/π2ππΆ;
60
βπ = 20π€/π2ππΆ; π(π‘) = 90ππΆ; π = 8800ππ/π3; ππ = 400π½/ππππΆ;
π = 360π€/πππΆ
Time required to cool the plate, π =?
Biot number,
π΅π =βπΏπ
π=
β (πΏ2)
π=
100 Γ (0.02/2)
360= 0.00277
Since, π΅π < 0.1, the internal resistance can be neglected and lumped capacitance
method may be applied for the solution of the problem.
Fig. (7.1)
The basic heat transfer equation can be written as:
ππ = βπππ
ππ‘
ππ= βπ€π΄π (π(π‘) β ππ€) + βππ΄π (π(π‘) β ππ)
= π΄π [βπ€(π(π‘) β ππ€) + βπ(π(π‘) β ππ)]
Where ππ€ and ππ are temperatures of water and air respectively and they are not
changing with time.
β΄ βπ π΄π πΏ ππ (ππ(π‘)
ππ) = π΄π [βπ€(π(π‘) β ππ€) + βπ(π(π‘) β ππ)]
Or
βπ πΏ ππ
ππ‘
ππ= π(π‘)(βπ€ + βπ) β (βπ€ππ€ + βπππ)
61
Or
ππ(π‘)
π(π‘)(βπ€ + βπ) β (βπ€ππ€ + βπππ)=
ππ
π πΏ ππ
Or
ππ(π‘)
π1π(π‘) β π2= β
ππ
π πΏ ππ
Where
π1 = βπ€ + βπ and π2 = βπ€ππ€ + βπππ
β΄ 1
π1β«
ππ(π‘)
π(π‘) βπ2
π1
= β β«ππ
π πΏ ππ
Or
1
π1β«
ππ(π‘)
π(π‘) βπ2
π1
= β β«ππ
π πΏ ππ
π
0
where π =π2
π1
π(π‘)
ππ
Or
1
π1
[ln(π(π‘) β π)]ππ
π(π‘)= β
π
π πΏ ππ
Or
1
π1
[ln(π(π‘) β π)]π(π‘)ππ =
π
π πΏ ππ
Or
π =π πΏ ππ
π1ln [
ππ β π
π(π‘) β π] (1)
π1 = βπ€ + βπ = 100 + 20 = 120
π2 = βπ€ππ€ + βπππ = 100 Γ 30 + 20 Γ 30 = 3600
π =π2
π1=
3600
120= 30
Substituting the proper values in equation (1), we get:
62
π =8800 Γ 0.02 Γ 400
120ln [
150 β 30
90 β 30] = 406.6 π or 6.776 minutes
7.3 Example (3): Determining the Conditions under which the Contact
Surface Remains at Constant Temperature
Two infinite bodies of thermal conductivities π1 and π2, thermal diffusivities πΌ1 and
πΌ2 are initially at temperatures π‘1 and π‘2 respectively. Each body has single plane
surface and these surfaces are placed in contact with each other. Determine the
conditions under which the contact surface remains at constant temperature π‘π where
π‘1 > π‘π > π‘2 .
Solution:
The rate of heat flow at a surface (π₯ = 0) is given by,
π =βππ΄βπ‘
βπ πΌ π
Heat received by each unit area of contact surface from the body at temperature π‘1 is,
π1 =βπ1(π‘1 β π‘π )
βπ πΌ1 π
Heat lost by each unit area of contact surface from the body at temperature π‘2 is,
π2 =βπ2(π‘π β π‘2)
βπ πΌ2 π
The contact surface will remain at a constant temperature if:
βπ1(π‘1 β π‘π )
βπ πΌ1 π=
βπ2(π‘π β π‘2)
βπ πΌ2 π
Or
π1(π‘1 β π‘π )
β πΌ1
=π2(π‘π β π‘2)
β πΌ2
Or
π1(π‘1 β π‘π )βπΌ2 = π2(π‘π β π‘2)βπΌ1
Or
π1π‘1βπΌ2 β π1π‘π βπΌ2 = π2π‘π βπΌ1 β π2π‘2βπΌ1
63
Or
π‘π (π1βπΌ2 + π2βπΌ1) = π1π‘1βπΌ2 + π2π‘2βπΌ1
Or
π‘π =π1π‘1βπΌ2 + π2π‘2βπΌ1
π1βπΌ2 + π2βπΌ1
By dividing the numerator and the denominator by βπΌ1 πΌ2, the following formula is
obtained:
π‘π =(π1π‘1/βπΌ1) + (π2π‘2/βπΌ2)
(π1/βπΌ1) + (π2/βπΌ2)
7.4 Example (4): Calculation of the Time Required for the Plate to
Reach a Given Temperature
A 50ππ Γ 50ππ copper slab 6.25mm thick has a uniform temperature of 300ππΆ. Its
temperature is suddenly lowered to 36ππΆ. Calculate the time required for the plate to
reach the temperature of 108ππΆ.
Take: π = 9000ππ/π3; ππ = 0.38ππ½/ππππΆ; π = 370π€/πππΆ and β = 90π€/π2ππΆ
Solution:
Surface area of plate (two sides),
π΄π = 2 Γ 0.5 Γ 0.5 = 0.5π2
Volume of plate,
π = 0.5 Γ 0.5 Γ 0.00625 = 0.0015625π3
Characteristic length,
πΏ =π
π΄π =
0.0015625
0.5= 0.003125 π
π΅π =βπΏ
π=
90 Γ 0.003125
370= 7.6 Γ 10β4
Since, π΅π βͺ 0.1 , hence lumped capacitance method (Newtonian heating or cooling)
may be applied for the solution of the problem.
64
The temperature distribution is given by:
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓ πΉπ
πΉπ =π
ππππΏ2β π =
370
9000 Γ 0.38 Γ 103 Γ 0.0031252β π = 11.0784 π
π
ππ=
108 β 36
300 β 36= πβ7.6Γ10β4Γ11.0784 π = πβ8.42Γ10β3 π
0.27273 = πβ8.42Γ10β3 π
ln 0.27273 = β8.42 Γ 10β3 π ln π
π =ln 0.27273
β8.42 Γ 10β3 ln π= 154.31 π
7.5 Example (5): Determination of the Time Required for the Plate to
Reach a Given Temperature
An aluminum alloy plate of 400ππ Γ 400ππ Γ 4ππ size at 200ππΆ is suddenly
quenched into liquid oxygen at β183ππΆ. Starting from fundamentals or deriving the
necessary expression, determine the time required for the plate to reach a temperature
of β70ππΆ. Assume β = 20000ππ½/π2 β βπ βπ πΆ
ππ = 0.8ππ½/ππππΆ , and π = 3000ππ/π3, π for aluminum at low temperature
may be taken as 214π€/πππΆ ππ 770.4 ππ½/πβππΆ
Solution:
Surface area of the plate,
π΄π = 2 Γ 0.4 Γ 0.4 = 0.32π2
Volume of the plate,
π = 0.4 Γ 0.4 Γ 0.004 = 0.00064π3
Characteristic length,
πΏ =π‘
2=
0.004
2= 0.002 π
65
Or πΏ =π
π΄π =
0.00064
0.32= 0.002 π
π for aluminum, at low temperature may be taken as 214π€/πππΆ or 770.4ππ½/πβππ
β΄ π΅π =βπΏ
π=
2000 Γ 0.002
770.4= 0.0519
Since, π΅π βͺ 0.1, hence lumped capacitance method may be applied for the solution
of the problem.
The temperature distribution is given by:
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
πΉπ =π
ππππΏ2β π =
214
3000 Γ 0.8 Γ 103 Γ 0.0022β π = 22.3 π
π΅π Γ πΉπ = 0.0519 Γ 22.3 = 1.15737 π
β΄π
ππ=
β70 β (β183)
200 β (β183)== πβ1.15737 π
113
383= πβ1.15737 π
0.295 = πβ1.15737 π
ln 0.295 = β1.15737 π ln π
π =ln 0.295
β1.15737 Γ 1= 1.055 π
7.6 Example (6): Determining the Temperature of a Solid Copper
Sphere at a Given Time after the Immersion in a Well β Stirred Fluid
A solid copper sphere of 10ππ diameter (π = 8954ππ/π3, ππ = 383π½/ππ, πΎ =
386π€/ππΎ) initially at a uniform temperature of ππ = 250ππΆ, is suddenly immersed
in a well β stirred fluid which is maintained at a uniform temperature πβ = 50ππΆ.
66
The heat transfer coefficient between the sphere and the fluid is β = 200π€/π2πΎ.
Determine the temperature of the copper block at π = 5 πππ. after the immersion.
Solution:
Given: π = 10ππ = 0.1π; π = 8954ππ/π3; ππ = 383π½/ππ π; π = 386π€/π πΎ,
ππ = 250ππΆ; πβ = 50ππΆ; β = 200π€/π2πΎ; π = 5πππ = 5 Γ 60 = 300 π
Temperature of the copper block, π(π‘) = ?
The characteristic length of the sphere is,
πΏ =π
π΄π =
43
ππ3
4ππ2=
π
3=
π
6=
0.1
6= 0.01667π
π΅π =βπΏ
π=
200 Γ 0.01667
386= 8.64 Γ 10β3
Since, π΅π βͺ 0.1 , hence lumped capacitance method (Newtonian heating or cooling)
may be applied for the solution of the problem.
The temperature distribution is given by:
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓ πΉπ
πΉπ =π
ππππΏ2β π =
386
8954 Γ 383 Γ 0.016672 Γ 300= 121.513
π΅π Γ πΉπ = 8.64 Γ 10β3 Γ 121.513 = 1.05
β΄π
ππ=
βπ(π‘) β 50
250 β 50= πβ1.05
π(π‘) β 50 = 200 πβ1.05
β΄ π(π‘) = 50 + 200 πβ1.05 = 50 + 70 = 120ππ
7.7 Example (7): Determination of the Heat Transfer Coefficient
An average convective heat transfer coefficient for flow of 90ππΆ air over a plate is
measured by observing the temperature β time history of a 40ππ thick copper slab
(π = 9000ππ/π3, ππ = 0.38ππ/ππππΆ, π = 370π€/πππΆ) exposed to 90ππΆ air. In
67
one test run, the initial temperature of the plate was 200ππΆ, and in 4.5 minutes the
temperature decreased by 35ππΆ. Find the heat transfer coefficient for this case.
Neglect internal thermal resistance.
Solution:
Given: πβ = 90ππΆ; π‘ = 40ππ ππ 0.04π; π = 9000ππ/π3; ππ = 0.38ππ/ππππΆ;
ππ = 200ππΆ; π(π‘) = 200 β 35 = 165ππΆ; π = 4.5πππ = 270π
Characteristic length of the sphere is,
πΏ =π‘
2=
0.04
2= 0.02π
π΅π =βπΏ
π=
0.02β
370= 5.405 Γ 10β5β
πΉπ =π
ππππΏ2β π =
370
9000 Γ 0.38 Γ 103 Γ 0.022Γ 270 = 73.03
π΅π Γ πΉπ = 5.405 Γ 10β5 Γ 73.03β = 394.73 Γ 10β5β = 0.003947β
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
π
ππ=
165 β 90
200 β 90= πβ0.003947β
0.682 = πβ0.003947β
ln 0.682 = β0.003947β ln π
β =ln 0.682
β0.003947 Γ 1= 96.97π€/π2π
πΆ
7.8 Example (8): Determination of the Heat Transfer Coefficient
The heat transfer coefficients for flow of air at 28ππΆ over a 12.5ππ diameter sphere
are measured by observing the temperature β time history of a copper ball of the same
dimension. The temperature of the copper ball (ππ = 0.4ππ/ππ πΎ and π =
8850ππ/π3) was measured by two thermo β couples, one located in the center and
68
the other near the surface. Both the thermocouples registered the same temperature at
a given instant. In one test the initial temperature of the ball was 65ππΆ, and in 1.15
minutes the temperature decreased by 11ππΆ . Calculate the heat transfer coefficient
for this case.
Solution:
Given: πβ = 28ππΆ; π(sphere) =12.5
2= 6.25ππ = 0.00625π; ππ = 0.4ππ/ππ πΎ;
π = 8850ππ/π3; ππ = 65ππΆ; π(π‘) = 65 β 11 = 54ππΆ; π = 1.15πππ = 69 π ;
π΅π =βπΏ
π; characteristic length πΏ =
π
π΄π =
π
3=
0.00625
3= 2.083 Γ 10β3
Since, heat transfer coefficient has to be calculated, so assume that the internal
resistance is negligible and π΅π is much less than 0.1 .
π΅π =βπ
3π=
0.00625β
3π=
2.083 Γ 10β3β
π
πΉπ =π
ππππΏ2β π =
π
8850 Γ 0.4 Γ 103 Γ (2.083 Γ 10β3)2Γ 270
= 0.0651 π Γ 69 = 4.5 π
π΅π Γ πΉπ =0.00625β
3πΓ 4.5π = 9.375 Γ 10β3β
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
π
ππ=
54 β 28
65 β 28= πβ9.375Γ10β3β
0.7027 = πβ0.009375β
ln 0.7027 = β0.009375β ln π
β΄ β =ln 0.7027
β0.009375 Γ 1= 37.63π€/π2πΎ
69
7.9 Example (9): Calculation of the Initial Rate of Cooling of a Steel
Ball
A steel ball 50mm in diameter and at 900ππΆ is placed in still atmosphere of 30ππΆ.
Calculate the initial rate of cooling of the ball in ππΆ/πππ, if the duration of cooling is
1 minute.
Take: π = 7800ππ/π3; ππ = 2ππ/ππππΆ (for steel); β = 30π€/π2ππΆ.
Neglect internal thermal resistance.
Solution:
Given: π =50
2= 25ππ = 0.025π; ππ = 900ππΆ; πβ = 30ππΆ; π = 7800ππ/π3
ππ = 2ππ/ππππΆ; β = 30π€/π2ππΆ; π = 1πππ = 60 π ;
The temperature variation in the ball (with respect to time), neglecting internal
thermal resistance, is given by:
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
π΅π =βπΏ
π, πΏ of a ball =
π
3=
0.025
3
β΄ π΅π =βπ
3π=
30 Γ 0.025
3π=
0.25
π
πΉπ =π
ππππΏ2β π =
π
7800 Γ 2 Γ 103 Γ (0.025/3)2β π
πΉπ = 9.23 Γ 10β4 Γ 60 = 0.0554π
π΅π Γ πΉπ =0.25
πΓ 0.0554π = 0.01385
π
ππ=
π(π‘) β 30
900 β 30= πβ0.01385
π(π‘) = 870 πβ0.01385 + 30 = 888ππΆ
β΄ rate of cooling = 900 β 888
1 πππ= 12ππΆ/πππ
70
7.10 Example (10): Determination of the Maximum Speed of a
Cylindrical Ingot inside a Furnace
A cylinder ingot 10ππ diameter and 30ππ long passes through a heat treatment
furnace which is 6m in length. The ingot must reach a temperature of 800ππΆ before it
comes out of the furnace. The furnace gas is at 1250ππΆ and the ingot initial
temperature is 90ππΆ. What is the maximum speed with which the ingot should move
in the furnace to attain the required temperature? The combined radiative and
convective surface heat transfer coefficient is 100π€/π2ππΆ.
Take: k (steel) = 40π€/π2ππΆ and πΌ (thermal diffusivity of steel) = 1.16 Γ 10β5π2/π .
Solution:
π = 10ππ = 0.1π; πΏ = 30ππ = 0.3π; Length of the furnace = 6π;
ππ = 800ππΆ; π(π‘) = 800ππΆ; πβ = 90ππΆ;
π£πππ₯ of ingot passing through the furnace =?
β = 100π€/π2ππΆ; π(steel) = 40π€/πππΆ; πΌ(steel) = 1.16 Γ 10β5π2/π
Characteristic length,
πΏπ =π
π΄π =
43
π2πΏ
[πππΏ +π4
π2 Γ 2]=
ππΏ
4πΏ + 2π
=0.1 Γ 0.3
4 Γ 0.3 + 2 Γ 0.1= 0.02143π
π΅π =βπΏπ
π=
100 Γ 0.02143
40= 0.0536
As π΅π βͺ 0.1 , Then internal thermal resistance of the ingot for conduction heat flow
can be neglected.
The time versus temperature relation is given as:
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
πΉπ =π
ππππΏ2β π =
πΌ
πΏ2β π =
1.16 Γ 10β5
0.021432β π = 0.02526 π
71
π΅π Γ πΉπ = 0.0536 Γ 0.02526 π = 1.35410β3π = 0.001354 π
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓ πΉπ
π
ππ=
800 β 90
1250 β 90= πβ0.001354 π
0.6121 = πβ0.001354 π
β0.001354 π ln π = ln 0.6121
π =ln 0.6121
β0.001354= 362.5 π
π£πππ₯ of ingot passing through the furnace,
π£πππ₯ =furnace length
time=
6
362.5= 0.01655π/π
7.11 Example (11): Determining the Time Required to Cool a Mild
Steel Sphere, the Instantaneous Heat Transfer Rate, and the Total
Energy Transfer
A 15ππ diameter mild steel sphere (π = 4.2π€/ππC is exposed to cooling air flow
at 20ππ resulting in the convective, coefficient β = 120π€/π2ππΆ.
Determine the following:
(i) Time required to cool the sphere from 550ππΆ to 90ππΆ .
(ii) Instantaneous heat transfer rate 2 minutes after the start of cooling.
(iii) Total energy transferred from the sphere during the first 2 minutes.
For mild steel take: π = 7850ππ/π3; ππ = 475π½/ππππΆ; and πΌ = 0.045 π2/β
Solution:
Given: π =15
2= 7.5ππ = 0.0075π; π = 42π€/π2π
πΆ; πβ = 20ππΆ; ππ = 550ππΆ;
π(π‘) = 90ππΆ; β = 120π€/π2ππΆ;
(i) Time required to cool the sphere from 550ππΆ to 90ππΆ, π = ?
The characteristic length, πΏπ is given by,
72
πΏπ =π
3=
0.0075
3= 0.0025π
Biot number,
π΅π =βπΏπ
π=
120 Γ 0.0025
42= 0.007143
Since, π΅π βͺ 0.1 , so we can use the lumped capacitance theory to solve this problem.
Fourier Number,
πΉπ =π
ππππΏ2β π =
πΌ
πΏπ2
β π
πΌ = 0.045π2/β =0.045
3600= 1.25 Γ 10β5π2/π
πΉπ =1.25 Γ 10β5
(0.0025)2β π = 2π
π΅π Γ πΉπ = 0.007143 Γ 2π
The temperature variation with time is given by:
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
=90 β 20
550 β 20= πβ0.014286 π
0.132 = πβ0.014286 π
β0.014286 π ln π = ln 0.132
π =ln 0.132
β0.014286= 141.7 π
(ii) Instantaneous heat transfer rate 2 minutes (0.0333h) after the start of cooling,
πβ²(π) =?
πβ²(π) = βπ΄π πππβπ΅πΓπΉπ
π΅π Γ πΉπ = 0.014286 Γ 2 Γ 60 = 1.7143
73
πβ²(π) = 120 Γ 4π Γ (0.0075)2(550 β 20)πβ1.7143 = 8.1π€
(iii) Total energy transferred from the sphere during the first 2 minutes, (0.0333h)
π(π‘) = ?
π(π‘) = βπ΄π ππ[1 β πβπ΅πΓπΉπ]π
π΅π Γ πΉπ
= 120 Γ 4π Γ (0.0075)2(550 β 20)[1 β πβ1.7143] Γ120
1.7143= 2580.2 π½
Or
πΉπ =π
ππππΏπ2
β π =π
7850 Γ 475 Γ 0.00252Γ 120 = 206
π΅π Γ πΉπ = 0.007143 Γ 206 = 1.471
π(π‘) = 120 Γ 4π Γ (0.0075)2(550 β 20)[1 β πβ1.471] Γ120
1.471= 2825 π½
7.12 Example (12): Estimation of the Time Required to Cool a
Decorative Plastic Film on Copper Sphere to a Given Temperature
using Lumped Capacitance Theory
The decorative plastic film on copper sphere 10mm in diameter is cured in an oven at
75ππΆ. After removal from oven, the sphere is exposed to an air stream at 10m/s and
23ππΆ. Estimate the time taken to cool the sphere to 35ππΆ using lumped capacitance
theory.
Use the following correlation:
ππ’ = 2 + [0.4(π π)0.5 + 0.06(π π)2/3](ππ)0.4 [ππ
ππ ]
0.25
For determination of correlation coefficient β, use the following properties of air and
copper:
For copper: π = 8933ππ/π3; π = 400π€/π πΎ; ππ = 380π½/ππππΆ
For air at 23ππΆ: ππ = 18.6 Γ 10β6ππ /π2, π = 15.36 Γ 10β6π2/π
π = 0.0258π€/π πΎ, ππ = 0.709, and
ππ = 19.7 Γ 10β6ππ /π2, at 35ππΆ
74
Solution:
π = 10ππ = 0.01π; ππ = 75ππΆ; π£ = 10π/π ; πβ = 23ππΆ; π(π‘) = 35ππΆ;
Time taken to cool the sphere, π = ?
π π =π£ π
π=
10 Γ 0.01
15.36 Γ 10β6= 6510
ππ’ = 2 + [0.4(6510)0.5 + 0.06(6510)2/3] Γ (0.709)0.4 Γ [18.16 Γ 10β6
19.78 Γ 10β6]
0.25
= 2 + [32.27 + 20.92] Γ 0.87 Γ 0.979 = 47.3
ππ ππ’ =β π
π= 47.3
β΄ β =π
πππ’ =
0.0258
0.01Γ 47.3 = 122π€/π2π
πΆ
The time taken to cool from 75ππΆ to 35ππΆ may be found from the following relation:
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
π΅π =β πΏ
π
The characteristic length of a sphere, πΏ = π
3=
0.005
3π
π΅π =β πΏ
π=
122 Γ 0.005
3 Γ 400= 5.083 Γ 10β4
Since, π΅π βͺ 0.1 , so we can use the lumped capacitance theory to solve this problem.
πΉπ =π
ππππΏ2β π =
400
8933 Γ 380 Γ (0.005
3 )2 β π = 42.421 π
π΅π Γ πΉπ = 5.083 Γ 10β4 Γ 42.421 π = 0.0216 π
π
ππ=
35 β 23
75 β 23= πβ0.0216 π
0.2308 = πβ0.0216 π
75
ln 0.2308 = β0.0216 π ln π
π =ln 0.2308
β0.0216= 67.9 β 68 π
7.13 Example (13): Calculation of the Time Taken to Boil an Egg
An egg with mean diameter of 40mm and initially at 20ππΆ is placed in a boiling
water pan for 4 minutes and found to be boiled to the consumer's taste. For how long
should a similar egg for the same consumer be boiled when taken from a refrigerator
at 5ππΆ. Take the following properties for eggs:
π = 10π€/πππΆ; π = 1200ππ/π3; ππ = 2ππ/ππππΆ; and
β (heat transfer coefficient) = 100π€/π2ππΆ.
Use lumped capacitance theory.
Solution:
Given: π =40
2= 20ππ = 0.02π; ππ = 20ππ; πβ = 100ππΆ; π = 4 Γ 60 = 240π ;
π = 10π€/πππΆ; π = 1200ππ/π3; ππ = 2ππ/ππππΆ; β = 100π€/π2ππΆ;
For using the lumped capacitance theory, the required condition π΅π βͺ 0.1 must be
valid.
π΅π =β πΏ
π , where L is the characteristic length which is given by,
πΏ =π
π΄π =
π
3=
0.02
3π
β΄ π΅π =β πΏ
π=
β Γ 0.02
π Γ 3=
100 Γ 0.02
10 Γ 3= 0.067
As π΅π βͺ 0.1 , we can use the lumped capacitance system.
The temperature variation with time is given by:
π(π‘) β πβ
ππ β πβ= πβπ΅πΓπΉπ
πΉπ =π
ππππΏ2β π =
10
1200 Γ 2 Γ 103 Γ (0.02
3 )2 Γ 240 = 22.5
76
π΅π Γ πΉπ = 0.067 Γ 22.5 = 1.5075
π(π‘) β 100
20 β 100= πβ1.5075
π(π‘) = 100 β 80 πβ1.5075 = 82.3ππΆ β 82ππΆ
Now, let us find π when the given data is: ππ = 5ππΆ; πβ = 100ππΆ and
π(π‘) = 82ππΆ.
82 β 100
5 β 100= πβπ΅πΓπΉπ
πΉπ =π
ππππΏ2β π =
10
1200 Γ 2 Γ 103 Γ (0.02
3 )2 β π = 0.09375 π
π΅π Γ πΉπ = 0.067 Γ 0.09375 π = 6.281 Γ 10β3π = 0.00628 π
0.1895 = πβ0.00628 π
β0.00628 π ln π = ln 0.1895
π =ln 0.1895
β0.00628= 264.9 π = 4.414 ππππ’π‘ππ
7.14 Example (14): Determining the Total Time Required for a
Cylindrical Ingot to be heated to a Given Temperature
A hot cylinder ingot of 50mm diameter and 200mm long is taken out from the
furnace at 800ππΆ and dipped in water till its temperature fall to 500ππΆ . Then, it is
directly exposed to air till its temperature falls to 100ππΆ. Find the total time required
for the ingot to reach the temperature from 800ππΆ to 100ππΆ. Take the following:
π(thermal conductivity of ingot) = 60π€/πππΆ;
π(specific heat of ingot) = 200π½/πππΆ;
π(density of ingot material) = 800ππ/π3;
βπ€(heat transfer coefficient in water) = 200π€/π2ππΆ;
77
βπ(heat transfer coefficient in air) = 20π€/π2ππΆ;
Temperature of air or water = 30ππΆ
Solution:
Given: π =50
2= 25ππ = 0.025π; πΏ = 200ππ or 0.2π
The characteristic length of a cylinder,
πΏπ =π
2=
0.025
2= 0.0125π
π΅π =β πΏ
π=
200 Γ 0.0125
60= 0.04167
As Bi is less than 0.1, the internal thermal resistance can be neglected, and lumped
capacitance theory can be used. The total time (π) can be calculated by calculating
π1 (time required in water) and π2 (time required in air) and adding them such that
π = π1 + π2
(a) The temperature variation with respect to time when cooled in water is given by:
(see Fig. (7.2) below)
Fig. (7.2) Temperature variation with time when the ingot is cooled in water
78
π(π‘) β ππ€
ππ β ππ€= πβπ΅πΓπΉπ
πΉπ =π
ππππΏ2β π1 =
60
800 Γ 200 Γ (0.0125)2β π1 = 2.4 π1
π΅π Γ πΉπ = 0.04167 Γ 2.4 π1 = 0.1 π1
β΄ π
ππ=
π(π‘) β ππ€
ππ β ππ€= πβπ΅πΓπΉπ
=500 β 30
800 β 30= πβ0.1 π1
0.61 = πβ0.1 π1
β0.1 π1 ln π = ln 0.61
π1 =ln 0.61
β0.1= 4.94 π
(b) The temperature variation with respect to time when cooled in air is given by: (see
Fig. (7.3) below)
Fig. (7.2) Temperature variation with time when the ingot is cooled in air
79
β΄ π
ππ=
π(π‘) β ππ
ππ β ππ= πβπ΅πΓπΉπ
π΅π =β πΏ
π=
20 Γ 0.0125
60= 0.004167
πΉπ =π
ππππΏ2β π2 = 2.4 π2
π΅π Γ πΉπ = 0.004167 Γ 2.4 π2 = 0.01 π2
π
ππ=
100 β 30
500 β 30=
70
470= πβ0.01 π2
0.149 = πβ0.01 π2
β0.01 π2 ln π = ln 0.149
β΄ π2 =ln 0.149
β0.01 Γ 1= 190.42 π
Total time (π) is given by:
π = π1 + π2 = 4.94 + 190.42 = 195.36 π = 3.256 πππ.
80
Chapter Eight
Unsolved Theoretical Questions and Further Problems in
Lumped Capacitance System
8.1 Theoretical Questions:
1. What is meant by transient heat conduction?
2. What is lumped capacity?
3. What are the assumptions for lumped capacity analysis?
4. What are Fourier and Biot numbers? What is the physical significance of these
numbers?
5. Define a semi β infinite body.
6. What is an error function? Explain its significance in a semi β infinite body in
transient state.
7. What are Heisler charts?
8. Explain the significance of Heisler charts in solving transient conduction problems.
8.2 Further Problems:
1. A copper slab (π = 9000ππ/π3, π = 380π½/ππππΆ, π = 370π€/πππΆ) measuring
400ππ Γ 400ππ Γ 5ππ has a uniform temperature of 250ππ. Its temperature is
suddenly lowered to 30ππΆ. Calculate the time required for the plate to reach the
temperature of 90ππΆ. Assume convective heat transfer coefficient as 90π€/π2ππΆ .
π¨ππ. {πππ. ππ π}
2. An aluminum alloy plate 0.2π2 surface area (both sides), 4mm thick and at 200ππΆ
is suddenly quenched into liquid oxygen which is at -183ππΆ . Find the time required
for the plate to reach the temperature of -70ππΆ .
Take: π = 2700ππ/π3, π = 890π½/ππππΆ, β = 500π€/π2ππΆ
π¨ππ. {ππ. ππ π }
3. A sphere of 200mm diameter made of cast iron initially at a uniform temperature
of 400ππ is quenched into oil. The oil bath temperature is 40ππΆ. If the temperature of
81
sphere is 100ππΆ after 5 minutes, find heat transfer coefficient on the surface of the
sphere.
Take: ππ (cast iron) =0.32πΎπ½/ππππΆ; π(cast iron) =7000kg/m3
Neglect internal thermal resistance.
π¨ππ. {πππππ/ππππͺ}
4. An average convective heat transfer coefficient for flow of 100ππΆ air over a flat
plate is measured by observing the temperature β time history of a 30 mm thick
copper slab (π = 9000ππ/π3, π = 0.38ππ½/ππππΆ, π = 370π€/πππΆ) exposed to
100ππΆ air. In one test run, the initial temperature of the plate was 210ππΆ and in 5
minutes the temperature decreased by 40ππΆ . Find the heat transfer coefficient for
this case. Neglect internal thermal resistance.
π¨ππ. {ππ. πππ/ππππͺ}
5. A cylinder steel ingot 150mm in diameter and 400mm long passes through a heat
treatment furnace which is 6m in length. The ingot must reach a temperature of
850ππΆ before it comes out of the furnace. The furnace gas is at 1280ππΆ and ingot
initial temperature is 100ππΆ. What is the maximum speed with which the ingot
should move in the furnace to attain the required temperature? The combined
radiative and convective surface heat transfer coefficient is 100π€/π2ππΆ. Take k
(steel)= 45π€/πππΆ and πΌ (thermal diffusivity) = 0.46 Γ 10β5π2/π .
π¨ππ. { π. πππ Γ ππβππ/π }
6. A hot mild steel sphere (π = 42.5π€/πππΆ) having 12mm diameter is planned to be
cooled by an air flow at 27ππΆ. The convective heat transfer coefficient is 114π€/
π2ππΆ. Determine the following:
(i) Time required to cool the sphere from 540ππΆ to 95ππΆ;
(ii) Instantaneous heat transfer rate 2 minutes after the start of cooling;
(iii) Total energy transferred from the sphere during the first 2 minutes. Take mild
steel properties as (π = 7850ππ/π3, π = 475ππ½/ππππΆ , πΌ = 0.043π2/β).
π¨ππ. { (π) π. πππ πππ; (ππ) π. ππππ ; (πππ) ππππ. π π±}
82
7. The heat transfer coefficients for the flow of 30ππΆ air over a 12.5mm diameter
sphere are measured from observing the temperature β time history of a copper ball
of the same dimensions. The temperature of the copper ball (π = 8930ππ/π3; π =
0.375ππ½/ππππΆ) was measured by two thermocouples, one located at the center and
the other near the surface. Both thermocouples registered within the accuracy of the
recording instruments the same temperature at the given instant, on one test run, the
initial temperature of the ball was 70ππΆ and in 1.15 minutes the temperature
decreased by 7ππΆ. Calculate the convective heat transfer coefficient for this case.
Ans. {πππ. π π/ππππͺ}
8. The temperature of an air stream flowing with a velocity of 3 m/s is measured by a
copper β constantan thermocouple which may be approximated as a sphere 3mm in
diameter. Initially the junction and air are at a temperature of 25ππΆ. The air
temperature suddenly changes to and is maintained at 200ππΆ.
i) Determine the time required for the thermocouple to indicate a temperature of
150ππΆ. Also determine the thermal time constant and temperature indicated by the
thermocouple at that instant;
ii) Discuss the suitability of this thermocouple to measure unsteady state temperature
of a fluid when the temperature variation in the fluid has a time period of 3 seconds.
The thermocouple junction properties are:
Density = 8685ππ/π3 ; specific heat π = 383 π/ππππΆ ; thermal conductivity
(thermocouple) π = 29π€/πππΆ and convective coefficient β = 150π€/π2ππΆ .
Ans. {ππ. ππ π; ππ. ππ π ; πππ. ππππͺ}
9. A 50 mm thick large steel plate (π = 42.5π€/πππΆ, πΌ = 0.043 π2/β), initially at
425ππΆ is suddenly exposed on both sides to an environment with convective heat
transfer coefficient 285π€/π2ππΆ and temperature 65ππΆ . Determine the center line
temperature and temperature inside the plate 12.5mm from the mid-plane after 3
minutes.
10. A long cylindrical bar (π = 17.5π€/πππΆ, πΌ = 0.0185 π2/β) of radius 75mm
comes out of oven at 815ππΆ throughout and is cooled by quenching it in a large bath
83
of 38ππΆ coolant. The surface coefficient of heat transfer between the bar surface and
the coolant is 175π€/π2ππΆ. Determine:
(i) The time taken by the shaft to reach 116ππΆ ;
(ii) The surface temperature of the shaft when its center temperature is 116ππΆ. Also
calculate the temperature gradient at the outside surface at the same instant of time.
Ans. {(π) πππππ; (ππ) ππ. πππͺ; πππππͺ/π}
11. A concrete highway may reach a temperature of 55ππΆ on a hot summer's day.
Suppose that a stream of water is directed on the highway so that the surface
temperature is suddenly lowered to 35ππΆ. How long will it take to cool the concrete
to 45ππΆ at a depth of 50mm from the surface?
For concrete take πΌ (thermal diffusivity) = 1.77 Γ 10β3π2/β
Ans. {π. ππ π}
12. It is proposed to bury water pipes underground in wet soil which is initially at
4.5ππΆ. The temperature of the surface of soil suddenly drops to β5ππΆ and remains at
this value for 10 hours. Determine the minimum depth at which the pipes be laid if
the surrounding soil temperature is to remain above 0ππΆ (without water getting
frozen). Assume the soil as semi β infinite soild.
For wet soil take πΌ (thermal diffusivity) = 2.78 Γ 10β3π2/β
Ans. {π. ππππ}
13. A 50 mm thick mild steel plate (πΌ = 1.25 Γ 10β5π2/π ) is initially at a
temperature of 40ππΆ. It is suddenly exposed on one side to a fluid which causes the
surface temperature to increase to and remain at 90ππΆ. Determine:
(i) The maximum time that the slab be treated as a semi β infinite body;
(ii) The temperature as the center of the slab one minute after the change in surface
temperature.
Ans. {(π) ππππ ; (ππ) ππππͺ}
14. The initial uniform temperature of a thick concrete wall (πΌ = 1.58 Γ 10β3π2/β;
π = 0.937π€/πππΆ) of a jet engine test cell is 21ππΆ. The surface temperature of the
84
wall suddenly rises to 315ππΆ when the combination of exhaust gases from the
turbojet and spray of cooling water occurs. Determine:
(i) The temperature at a point 75 mm from the surface after 7.5 hours;
(ii) The instantaneous heat flow rate at the specified plane and at the surface itself at
the instant mentioned at (i).
Use the solution for semi β infinite solid.
Ans. {(π) πππππͺ; (ππ) β ππππ. ππ/ππ; βπππππ/ππ}
15. The initial uniform temperature of a large mass of material (πΌ = 0.41 π2/β) is
120ππΆ. The surface of the material is suddenly exposed to and held permanently at
5ππΆ. Calculate the time required for the temperature gradient at the surface to reach
350ππΆ/π.
Ans. {ππππ}
16. A motor car of mass 1500 kg travelling at 80 km/h is brought to rest within a
period of 5 seconds when brakes are applied. The braking system consists of 4 brakes
with each brake band of 350 ππ2 area; these press against steel drum of equivalent
area. The brake lining and the drum surfaces (π = 55π€/πππΆ, πΌ = 1.24 Γ
10β5π2/π ) are at the same temperature and the heat generated during the stoppage
action dissipates by flowing across drums. If the drum surface is treated as semi β
infinite plate, calculate the maximum temperature rise.
Ans. {πππ. ππππͺ}
17. During periodic heating and cooling of a thick brick wall, the wall temperature
varies sinusoidally. The surface temperature ranges from 25ππΆ to 75ππΆ during a
period of 24 hours. Determine the time lag of the temperature wave corresponding to
a point located at 250 mm from the wall surface. The properties of the wall material
are: (π = 1620ππ/π3, π = 450π½/ππππΆ, π = 0.62π€/πππΆ).
Ans. {π. ππ π}
18. A single cylinder (πΌ = 0.042 π2/β from cylinder material) two β stroke I.C.
engine operates at 1500 π. π. π. Calculate the depth where the temperature wave due
to variation of cylinder temperature is damped to 1% of its surface value.
85
Ans. {π. πππ ππ}
19. The temperature distribution across a large concrete slab (π = 1.2π€/πππΆ, πΌ =
1.77 Γ 10β3π2/β) 500 mm thick heated from one side as measured by
thermocouples approximates to the relation: π‘ = 60 β 50π₯ + 12π₯2 + 20π₯3 β 15π₯4
where π‘ is in oπΆ and π₯ is in meters. Considering an area of 5π2, compute the
following:
(i) The heat entering and leaving the slab in unit time;
(ii) The heat energy stored in unit time;
(iii) The rate of temperature change at both sides of the slab; and
(iv) The point where the rate of heating or cooling is maximum.
Ans. {(π) ππππ, πππ π; (ππ) ππππ; (πππ) ππ. ππ Γ ππβπππ/π, ππ. ππ Γ
ππβπππ/π; (ππ) π. πππ}
86
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89
Appendix
Mathematical Formulae Summary
1. Conduction of heat in unsteady state refers to the transient conditions where in heat
flow and the temperature distribution at any point of the system vary continuously
with time.
2. The process in which the internal resistance is assumed negligible in comparison
with its surface resistance is called the Newtonian heating or cooling process.
π
ππ=
π(π‘) β πβ
ππ β πβ= π
ββπ΄π ππππ
βπ (π)
Where,
π = density of the solid, ππ/π3
π = volume of the body, π3
ππ = specific heat of the body, π½/ππππΆ ππ π½/ππ πΎ
β = heat transfer coefficient of the surface, π€/π2ππΆ ππ π€/π2πΎ
π΄π = surface area of the body, π2
π(π‘) = temperature of the body at any time, ππ
πβ = ambient temperature, ππ
π = time, π
Biot number,
π΅π =βπΏπ
π
Fourier number,
πΉπ =πΌ π
πΏπ2
Where,
πΏπ = characteristic length, or characteristic linear dimension.
πΌ = [π
π ππ] = thermal diffusivity of the solid.
90
π
ππ=
π(π‘) β πβ
ππ β πβ= πβπ΅πΓ πΉπ (ππ)
Instantaneous heat flow rate:
πβ²(π) = ββπ΄π (ππ β πβ)πβπ΅πΓπΉπ (πππ)
Total or cumulative heat transfer:
π(π‘) = ππ ππ(ππ β πβ)[πβπ΅πΓπΉπ β 1] (ππ£)
3. Time constant and response of temperature measuring instruments:
The quantity ππ ππ
βπ΄π is called time constant (πβ).
π
ππ=
π(π‘) β πβ
ππ β πβ= πβ(π/πβ)
The time required by a thermocouple to reach its 63.2% of the value of the initial
temperature difference is called its sensitivity.
4. Transient heat conduction in semi β infinite solids (β or π΅π β β): The temperature
distribution at any time π at a plane parallel to and at a distance π₯ from the surface
is given by:
π(π‘) β πβ
ππ β πβ= πππ [
π₯
2βπΌ π] (π)
Where πππ [π₯
2βπΌ π] is known as "Gaussian error function".
The instantaneous heat flow rate at a given x β location within the semi β infinite
body at a specified time is given by:
ππ = βππ΄(ππ β πβ)π[βπ₯2/4πΌπ]
βπ πΌ π (ππ)
The heat flow rate at the surface (π₯ = 0) is given by:
ππ π’πππππ == βππ΄(ππ β πβ)
βπ πΌ π (πππ)
The heat flow rate π(π‘) is given by:
92
Author
Osama Mohammed Elmardi Suleiman was born in Atbara,
Sudan in 1966. He received his diploma degree in mechanical
engineering from Mechanical Engineering College, Atbara,
Sudan in 1990. He also received a bachelor degree in
mechanical engineering from Sudan University of Science and
Technology β Faculty of Engineering in 1998, and a master
degree in solid mechanics from Nile Valley University (Atbara, Sudan) in 2003. He
contributed in teaching some subjects in other universities such as Red Sea
University (Port Sudan, Sudan), Kordofan University (Obayied, Sudan), Sudan
University of Science and Technology (Khartoum, Sudan) and Blue Nile University
(Damazin, Sudan). In addition, he supervised more than hundred and fifty under
graduate studies in diploma and B.Sc. levels and about fifteen master theses. He is
currently an assistant professor in department of mechanical engineering, Faculty of
Engineering and Technology, Nile Valley University. His research interest and
favorite subjects include structural mechanics, applied mechanics, control
engineering and instrumentation, computer aided design, design of mechanical
elements, fluid mechanics and dynamics, heat and mass transfer and hydraulic
machinery. He also works as a consultant and technical manager of Al β Kamali
workshops group for small industries in Atbara old and new industrial areas.