We look at the case of radial heat flow. Again, in radial heat flow, the temperature profiles that satisfy the boundary and initial conditions are the exponential and hyperbolic functions as derived in literature of conduction in fins. We use the technique of transforming the PDE into an integral equation. But in the case of radial heat flow, we have to multiply through by r the heat equation and then introduce integrals. We do this to avoid introducing integrals of the form of the exponential integral whose solutions cannot be expressed in the form of a simple mathematical function. We look at the case of a semi-infinite hollow cylinder for both insulated and non-insulated cases and then find the solution. We also look at cases of finite radius hollow cylinders subject to given boundary conditions. We notice that the solutions got for finite radius hollow cylinders do not reduce to those of semi-infinite hollow cylinders. We conclude by saying that this same analysis can be extended to spherical co-ordinates heat conduction.
Adaptive Restore algorithm & importance Monte Carlo
Β
RADIAL HEAT CONDUCTION SOLVED USING THE INTEGRAL EQUATION .pdf
1. Using the integral heat equation
Wasswa Derrick 4/27/24 Applied Mathematics
2.
3. TABLE OF CONTENTS
PREFACE ............................................................................................................................................3
RADIAL HEAT CONDUCTION WITH NO LATERAL CONVECTION...................................4
CASE1: SEMI-INFINITE HOLLOW CYLINDER...........................................................................................4
CASE 2: FIXED END TEMPERATURE ......................................................................................................9
CASE3: CONVECTION AT THE FREE END .............................................................................................16
CASE4: ZERO CONVECTION AT THE FREE END ....................................................................................24
RADIAL HEAT CONDUCTION WITH LATERAL CONVECTION........................................30
CASE1: SEMI-INFINITE CASE...............................................................................................................31
CASE2: CONVECTION AT THE FREE END .............................................................................................34
CONCLUSION...................................................................................................................................43
REFERENCES..................................................................................................................................44
4. PREFACE
We look at the case of radial heat flow. Again, in radial heat flow, the
temperature profiles that satisfy the boundary and initial conditions are the
exponential and hyperbolic functions as derived in literature of conduction in
fins. We use the technique of transforming the PDE into an integral equation.
But in the case of radial heat flow, we have to multiply through by r the heat
equation and then introduce integrals. We do this to avoid introducing
integrals of the form of the exponential integral whose solutions cannot be
expressed in the form of a simple mathematical function. We look at the case of
a semi-infinite hollow cylinder for both insulated and non-insulated cases and
then find the solution. We also look at cases of finite radius hollow cylinders
subject to given boundary conditions. We notice that the solutions got for finite
radius hollow cylinders do not reduce to those of semi-infinite hollow cylinders.
We conclude by saying that this same analysis can be extended to spherical co-
ordinates heat conduction.
5. RADIAL HEAT CONDUCTION WITH NO LATERAL
CONVECTION
CASE1: SEMI-INFINITE HOLLOW CYLINDER.
The governing PDE is:
πΆ
ππ
π»
πππ
+ πΆ
π
π
ππ»
ππ
=
ππ»
ππ
The boundary conditions are
π = ππ ππ‘ π = π1
π = πβ ππ‘ π = β
The initial condition is:
π = πβ ππ‘ π‘ = 0
The temperature profile that satisfies the conditions above is
π β πβ
ππ β πβ
= π
β(πβπ1)
πΏ
We transform the equation above into an integral equation and take integrals
with limits from π = π1 to π = π = β.
πΌ
π2
π
ππ2
+ πΌ
1
π
ππ
ππ
=
ππ
ππ‘
We take integrals and get
6. πΌ β«
π2
π
ππ2
ππ
π
π1
+ πΌ β« [
1
π
ππ
ππ
]ππ
π
π1
=
π
ππ‘
β« (π)ππ
π
π1
Where:
π = β
Let us look at the integral below:
β« [
1
π
ππ
ππ
]ππ
π
π1
ππ
ππ
= β
ππ β πβ
πΏ
π
β(πβπ1)
πΏ
β« [
1
π
ππ
ππ
]ππ
π
π1
= β β« [
1
π
ππ β πβ
πΏ
π
β(πβπ1)
πΏ ]ππ
π
π1
Upon rearranging, we get:
β« [
1
π
ππ
ππ
]ππ
π
π1
= β
ππ β πβ
πΏ
π
π1
πΏ β« [
1
π
π
βπ
πΏ ]ππ
π
π1
Calling
π’ =
π
πΏ
π = π’πΏ
ππ = πΏππ’
So, we have
β« [
1
π
ππ
ππ
]ππ
π
π1
= β
ππ β πβ
πΏ
π
π1
πΏ β« [
1
π’
πβπ’
]ππ’
π
π’
π1
πΏ
This integral is in the form of the Exponential integral i.e.,
β«[
1
π₯
πβπ₯
]ππ’ = πΈπ(βπ₯) + π
and is a non-elementary function. This means that the integral cannot be
expressed as a simple function. To avoid this problem, we have to multiply
through by r the heat equation as shown below and solve.
πΌ β« (π
π2
π
ππ2
)ππ
π
π1
+ πΌ β« [
ππ
ππ
]ππ
π
π1
=
π
ππ‘
β« (ππ)ππ
π
π1
Let us evaluate:
8. Now let us evaluate:
β« (ππ)ππ
π =β
π1
π = (ππ β πβ)π
β(πβπ1)
πΏ + πβ
β« (ππ)ππ
π =β
π1
= (ππ β πβ) β« (ππ
β(πβπ1)
πΏ )ππ
π =β
π1
+ β« πβππ
π =β
π1
= πΏ(ππ β πβ) + πβ(π β π1)
β« (ππ
β(πβπ1)
πΏ )ππ
π =β
π1
= π1πΏ + πΏ2
β« (ππ)ππ
π =β
π1
= (ππ β πβ)(π1πΏ + πΏ2) + πβ(π β π1)
Upon substituting all the above in the integral heat equation, we get
πΌ [
(ππ β πβ)
πΏ
(π1 + πΏ) β (ππ β πβ)] =
π
ππ‘
[(ππ β πβ)(π1πΏ + πΏ2
) + πβ(π β π1)]
But
π(πβ(π β π1))
ππ‘
= 0 π ππππ πβ πππ (π β π1) πππ ππππ π‘πππ‘π
So, we are left with
πΌ [
(ππ β πβ)
πΏ
(π1 + πΏ) β (ππ β πβ)] =
π
ππ‘
[(ππ β πβ)(π1πΏ + πΏ2
)]
πΌ [
1
πΏ
(π1 + πΏ) β 1] =
π
ππ‘
[(π1πΏ + πΏ2
)]
Upon substitution, we get
πΌ
π1
πΏ
= (π1 + 2πΏ)
ππΏ
ππ‘
The boundary condition is:
πΏ = 0 ππ‘ π‘ = 0
So, we get:
πΌπ1 β« ππ‘
π‘
0
= β« (π1πΏ + 2πΏ2)
πΏ
0
ππΏ
Upon simplification, we get:
9. πΌπ1π‘ =
π1πΏ2
2
+
2πΏ3
3
We get:
6πΌπ1π‘ = 3π1πΏ2
+ 4πΏ3
i.e.,
ππππΉπ
+ ππΉπ
β ππΆπππ = π
Which is a cubic function and can be solved to get πΏ as a function of time t.
You notice that the initial condition is satisfied for the above temperature
profile.
We can also go ahead and look at situations where there is natural convection
and other situations where the radius r is finite and not infinite.
10. CASE 2: FIXED END TEMPERATURE
The initial and boundary conditions are:
π» = π»β ππ π = π
π» = π»ππ β π»β ππ π = π
π» = π»ππ β π»β ππ π = π³
We start with a temperature profile below:
π β πβ = π΄π
π₯
πΏ + π΅π
βπ₯
πΏ
We evaluate the constants A and B using the boundary conditions and get the
temperature profile below:
π β πβ
ππ1 β πβ
=
(
ππ2 β πβ
ππ1 β πβ
) π ππβ
π₯
πΏ
+ π ππβ
πΏ β π₯
πΏ
π ππβ
πΏ
πΏ
The temperature profile above can be referenced in textbooks for heat flow in
extended surfaces like in the book [1].
To transform the above equation to cylindrical co-ordinates, we use the
substitutions,
πΏ = (π2 β π1)
And
π₯ = π β π1
And the temperature profile becomes:
π β πβ
ππ1 β πβ
=
(
ππ2 β πβ
ππ1 β πβ
)π ππβ
π β π1
πΏ
+ π ππβ
π2 β π
πΏ
π ππβ
π2 β π1
πΏ
The governing PDE is:
πΆ
ππ
π»
πππ
+ πΆ
π
π
ππ»
ππ
=
ππ»
ππ
The initial and boundary conditions are:
π» = π»β ππ π = π
15. Collecting like terms we have
πΌ
πΏ
((π2 + π1)cosh(
π2 β π1
πΏ
) β (π2 + π1)) =
ππΏ
ππ‘
((π2 + π1)cosh(
π2 β π1
πΏ
) β (π2 + π1))
The like terms of ((π2 + π1)cosh (
π2βπ1
πΏ
) β (π2 + π1)) cancel out and we remain with
πΌ
πΏ
=
ππΏ
ππ‘
Hence, we have
πΏ = β2πΌπ‘
Hence the temperature profile is:
π β πβ
ππ1 β πβ
=
(
ππ2 β πβ
ππ1 β πβ
)π ππβ
π β π1
πΏ
+ π ππβ
π2 β π
πΏ
π ππβ
π2 β π1
πΏ
Or
π β πβ
ππ1 β πβ
=
(
ππ2 β πβ
ππ1 β πβ
)π ππβ
π β π1
β2πΌπ‘
+ π ππβ
π2 β π
β2πΌπ‘
π ππβ
π2 β π1
β2πΌπ‘
In steady state, π‘ β β π π πΏ β β
Upon substitution we get
π β πβ
ππ1 β πβ
=
(
ππ2 β πβ
ππ1 β πβ
)π ππβ
π β π1
β
+ π ππβ
π2 β π
β
π ππβ
π2 β π1
β
π β πβ
ππ1 β πβ
=
(
ππ2 β πβ
ππ1 β πβ
) π ππβ0 + π ππβ0
π ππβ0
π β πβ
ππ1 β πβ
=
0
0
Lβhopitalβs rule is then invoked i.e.,
πππ
π₯ β π
π(π₯)
π(π₯)
=
πππ
π₯ β π
πβ²
(π₯)
πβ²(π₯)
We differentiate the numerate and denominator with respect to
1
πΏ
since it is the
one varying and we get
16. π β πβ
ππ1 β πβ
=
(
ππ2 β πβ
ππ1 β πβ
)π ππβ
π β π1
πΏ
+ π ππβ
π2 β π
πΏ
π ππβ
π2 β π1
πΏ
π β πβ
ππ1 β πβ
=
π β π1
πΏ
(
ππ2 β πβ
ππ1 β πβ
) πππ β
π β π1
πΏ
+ (
π2 β π
πΏ
)πππ β
π2 β π
πΏ
π2 β π1
πΏ
πππ β
π2 β π1
πΏ
Upon simplification, we get
π β πβ
ππ1 β πβ
=
π β π1
πΏ
(
ππ2 β πβ
ππ1 β πβ
) πππ β
π β π1
πΏ
+ (
π2 β π
πΏ
)πππ β
π2 β π
πΏ
π2 β π1
πΏ
πππ β
π2 β π1
πΏ
π β πβ
ππ1 β πβ
=
(π β π1) (
ππ2 β πβ
ππ1 β πβ
) πππ β
π β π1
πΏ
+ (π2 β π)πππ β
πΏ β π₯
πΏ
(π2 β π1)πππ β
π2 β π1
πΏ
We then substitute
πΏ = β2πΌπ‘ = β
And get
π β πβ
ππ1 β πβ
=
(π β π1) (
ππ2 β πβ
ππ1 β πβ
) + (π2 β π)
(π2 β π1)
Upon substitution, we get:
π» β π»β
π»ππ β π»β
=
(π β ππ) (
π»ππ β π»β
π»ππ β π»β
) + (ππ β π)
(ππ β ππ)
Hence, we get a temperature profile linear in radius r in steady state but this
temperature profile is in contrast to the logarithmic temperature profile expected.
So, we have to choose which theory we take to be true.
The other thing we notice is that the solution we have got doesnβt reduce to the
one of the semi-infinite solution when the radius π2 tends to infinity.
17. CASE3: CONVECTION AT THE FREE END
This same analysis can be extended to a metal rod with convection at the other
end of the metal rod where the temperature profile is given by [1]:
π β πβ
ππ β πβ
=
cosh[π(πΏ β π₯)] + (
βπΏ
ππ
) sinh[π(πΏ β π₯)]
cosh ππΏ + (
βπΏ
ππ
) π ππβππΏ
Or
π β πβ
ππ β πβ
=
cosh [
(πΏ β π₯)
πΏ
] + (
βπΏπΏ
π
) sinh[(
πΏ β π₯
πΏ
)]
cosh
πΏ
πΏ
+ (
βπΏπΏ
π
) π ππβ
πΏ
πΏ
For cylindrical co-ordinates we make the substitutions
πΏ = (π2 β π1)
And
π₯ = π β π1
And the temperature profile becomes:
π β πβ
ππ β πβ
=
cosh[π(π2 β π)] + (
βπ2
ππ
) sinh[π(π2 β π)]
cosh π(π2 β π1) + (
βπ2
ππ
) π ππβπ(π2 β π1)
The boundary and initial conditions are:
π» = π»π ππ π = ππ
βπ
π π»
π π
= πππ
(π» β π»β) ππ π = ππ
π» = π»β ππ π = π
This same analysis can be extended to a metal rod with convection at the other
end of the metal rod where the temperature profile is given by [1]:
π β πβ
ππ β πβ
=
cosh[π(π2 β π)] + (
βπ2
ππ
) sinh[π(π2 β π)]
cosh π(π2 β π1) + (
βπ2
ππ
) π ππβπ(π2 β π1)
Or
18. π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
] + (
βπ2
πΏ
π
) sinh[
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
To show that the initial condition is satisfied we assume from the above that
ππ‘ π‘ = 0, πΏ = 0.
π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
] + (
βπ2
πΏ
π
) sinh[
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
Becomes:
π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
=
π
(π2βπ)
πΏ + π
β(π2βπ)
πΏ
π
π2βπ1
πΏ + π
β(π2βπ1)
πΏ
π
β(π2βπ)
πΏ = πβ
(π2βπ)
0 = πββ(πΏβπ₯)
= 0
Similarly
π
β(π2βπ1)
πΏ = π
β(π2βπ1)
0 = πββ(π2βπ1)
= 0
So, we are left with
π β πβ
ππ β πβ
=
π
(π2βπ)
πΏ
π
π2βπ1
πΏ
= π
β(πβπ1)
πΏ = π
β(πβπ1)
0 = πββ(πβπ1)
= 0
Hence at π‘ = 0, π = πβ and hence the initial condition.
We use this temperature profile which satisfies the initial condition to solve the
heat equation and get πΏ as shown below:
Boundary and initial conditions are:
π» = π»π ππ π = ππ
βπ
π π»
π π
= πππ
(π» β π»β) ππ π = ππ
π» = π»β ππ π = π
The governing temperature profile is:
22. π
ππ‘
β« (ππ)ππ
π2
π1
β« (ππ)ππ
π2
π1
π = π΄ cosh [
(π2 β π)
πΏ
] + Bsinh [
(π2 β π)
πΏ
] + πβ
β« (ππ)ππ
π2
π1
= π΄ β« (π cosh [
(π2 β π)
πΏ
]) ππ
π2
π1
+ π΅ β« (ππ ππβ (
π2 β π
πΏ
)) ππ
π2
π1
+ πβ(π2 β π1)
But we have already evaluated the above so we get:
β« (ππ)ππ
π2
π1
= [π΄ (π1πΏ sinh (
π2 β π1
πΏ
) + πΏ2
[cosh (
π2 β π1
πΏ
) β 1]) + π΅ (π1πΏ cosh (
π2 β π1
πΏ
) β π2πΏ + πΏ2
sinh (
π2 β π1
πΏ
))] + πβ(π2 β π1)
Substituting all the above in the integral equation, we get
πΌ [
π΄π1
πΏ
sinh (
π2 β π1
πΏ
) +
π΅π1
πΏ
cosh (
π2 β π1
πΏ
) β
π΅π2
πΏ
] =
π
ππ‘
[π΄ (π1πΏ sinh (
π2 β π1
πΏ
) + πΏ2
[cosh (
π2 β π1
πΏ
) β 1]) + π΅ (π1πΏ cosh (
π2 β π1
πΏ
) β π2πΏ + πΏ2
sinh (
π2 β π1
πΏ
))]
Now let us collect like terms i.e., let us collect terms in A separately and terms
in B separately and get
πΌ
π΄π1
πΏ
sinh (
π2 β π1
πΏ
) =
π
ππ‘
[π΄ (π1πΏ sinh (
π2 β π1
πΏ
) + πΏ2 [cosh (
π2 β π1
πΏ
) β 1])]
Cancelling out A we get:
πΌ [
π1
πΏ
sinh (
π2 β π1
πΏ
)] =
π
ππ‘
[(π1πΏ sinh (
π2 β π1
πΏ
) + πΏ2 [cosh (
π2 β π1
πΏ
) β 1])] β¦ β¦ β¦ π΄
Similarly for terms in B
πΌ [
π΅π1
πΏ
cosh (
π2 β π1
πΏ
) β
π΅π2
πΏ
] =
π
ππ‘
[π΅ (π1πΏ cosh (
π2 β π1
πΏ
) β π2πΏ + πΏ2
sinh (
π2 β π1
πΏ
))]
Cancelling out B we get:
πΌ [
π1
πΏ
cosh (
π2 β π1
πΏ
) β
π΅π2
πΏ
] =
π
ππ‘
[(π1πΏ cosh (
π2 β π1
πΏ
) β π2πΏ + πΏ2
sinh (
π2 β π1
πΏ
))]β¦ β¦ π΅
Adding equations M and N we get:
πΌ [
π1
πΏ
(sinh (
π2 β π1
πΏ
) + cosh (
π2 β π1
πΏ
)) β
π2
πΏ
] =
π
ππ‘
[(π1πΏ (sinh (
π2 β π1
πΏ
) + cosh (
π2 β π1
πΏ
)) + πΏ2
[sinh (
π2 β π1
πΏ
) + cosh (
π2 β π1
πΏ
)] β πΏ(πΏ + π2))]
Now let us collect terms in sinh (
π2βπ1
πΏ
) + cosh (
π2βπ1
πΏ
) and get
πΌ [
π1
πΏ
(sinh(
π2 β π1
πΏ
) + cosh (
π2 β π1
πΏ
))] =
π
ππ‘
[(π1πΏ (sinh(
π2 β π1
πΏ
) + cosh(
π2 β π1
πΏ
)) + πΏ2
[sinh(
π2 β π1
πΏ
) + cosh(
π2 β π1
πΏ
)])]
23. Let us drop out the common term sinh (
π2βπ1
πΏ
) + cosh (
π2βπ1
πΏ
) and get
πΌ [
π1
πΏ
] =
π
ππ‘
[(π1πΏ + πΏ2)] β¦ . . π±
Let us also collect out the π2 terms and get:
πΌ [β
π2
πΏ
] =
π
ππ‘
[(βπΏ(πΏ + π2))]
Upon simplification we get:
πΌ [
π2
πΏ
] =
π
ππ‘
[(πΏ2
+ π2πΏ)]β¦ . . π²
Let us subtract equation K from equation J and get:
πΌ [
π2 β π1
πΏ
] =
π
ππ‘
[(π2 β π1)πΏ]
Upon simplification, we get:
πΌ
πΏ
=
ππΏ
ππ‘
The boundary conditions are:
πΏ = 0 ππ‘ π‘ = 0
Upon integrating, we get
πΌ β« ππ‘
π‘
0
= β« πΏππΏ
πΏ
0
We finally get
πΏ = β2πΌπ‘
Upon substitution in the temperature profile we get,
π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
] + (
βπ2
πΏ
π
) sinh[
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
π» β π»β
π»π β π»β
=
ππ¨π¬π‘ [
(ππ β π)
βππΆπ
] + (
πππ
βππΆπ
π
) π¬π’π§π‘[
(ππ β π)
βππΆπ
]
ππ¨π¬π‘
(ππ β ππ)
βππΆπ
+ (
πππ
βππΆπ
π
)ππππ
(ππ β ππ)
βππΆπ
24. Lβhopitalβs rule can be used to find the steady state temperature when time
tends to infinity.
Again, we notice that the temperature profile above doesnβt reduce to the semi-
infinite temperature profile when π2 tends to infinity because both solutions
have different values of πΏ.
25. CASE4: ZERO CONVECTION AT THE FREE END
The boundary and initial conditions are:
π» = π»π ππ π = ππ
π π»
π π
= π ππ π = ππ
π» = π»β ππ π = π
Recall the compact temperature profile that satisfies the boundary and initial
conditions is [2]:
π β πβ
ππ β πβ
=
cosh (
π2 β π
πΏ
)
cosh (
π2 β π1
πΏ
)
πΌ
π2
π
ππ2
+ πΌ
1
π
ππ
ππ
=
ππ
ππ‘
So, the temperature profile we are going to use is:
π» β π»β = π¨ ππ¨π¬π‘ (
ππ β π
πΉ
)
Where:
π΄ =
(ππ β πβ)
cosh
(π2 β π1)
πΏ
Multiplying through by r the heat equation becomes:
πΌπ
π2
π
ππ2
+ πΌ
ππ
ππ
=
πππ
ππ‘
Transforming the PDE into an integral equation, we get:
πΌ [β« (π
π2
π
ππ2
) ππ
π2
π1
+ β« [
ππ
ππ
] ππ
π2
π1
] =
π
ππ‘
β« (ππ)ππ
π2
π1
Let us evaluate the integral
β« (π
π2
π
ππ2
)ππ
π2
π1
28. Substituting all the above in the integral equation, we get
πΌ [
π΄π1
πΏ
sinh (
π2 β π1
πΏ
)] =
π
ππ‘
[π΄ (π1πΏ sinh (
π2 β π1
πΏ
) + πΏ2 [cosh (
π2 β π1
πΏ
) β 1])]
Now let us collect like terms i.e., let us collect terms in A separately and get:
πΌ
π΄π1
πΏ
sinh (
π2 β π1
πΏ
) =
π
ππ‘
[π΄ (π1πΏ sinh (
π2 β π1
πΏ
) + πΏ2 [cosh (
π2 β π1
πΏ
) β 1])]
Cancelling out A we get:
πΌ [
π1
πΏ
sinh (
π2 β π1
πΏ
)] =
π
ππ‘
[(π1πΏ sinh (
π2 β π1
πΏ
) + πΏ2 [cosh (
π2 β π1
πΏ
) β 1])]
Here is the catch lets us expand sinh (
π2βπ1
πΏ
) and cosh (
π2βπ1
πΏ
) into exponentials
and get:
Calling
π½ =
π2 β π1
πΏ
πΌ [
π1
πΏ
sinh π½] =
π
ππ‘
[(π1πΏ sinh π½ + πΏ2[coshπ½ β 1])]
Now we have:
πΌ [
π1
πΏ
(
ππ½
β πβπ½
2
)] =
π
ππ‘
[(π1πΏ(
ππ½
β πβπ½
2
) + πΏ2 [(
ππ½
+ πβπ½
2
) β 1])]
Collecting like terms i.e., terms in ππ½
and πβπ½
and constant terms and get:
πΌ [
π1
πΏ
(
ππ½
2
)] =
π
ππ‘
[(π1πΏ(
ππ½
2
) + πΏ2
(
ππ½
2
))]
Dropping out ππ½
we get:
πΌ [
π1
πΏ
] =
π
ππ‘
[(π1πΏ + πΏ2)] β¦ . π΄
Similarly collecting terms in πβπ½
we get:
πΌ [
π1
πΏ
(
βπβπ½
2
)] =
π
ππ‘
[(π1πΏ(
βπβπ½
2
) + πΏ2 [(
+πβπ½
2
)])]
Dropping out the πβπ½
we get:
29. πΌ [
π1
πΏ
] =
π
ππ‘
[(π1πΏ β πΏ2)] β¦ β¦ π΅
Collecting out the βconstantβ terms we have:
0 =
π
ππ‘
[(βπΏ2)]
So, what we have is
π
ππ‘
[(πΏ2)] = 0 β¦ π·
We are going to substitute equation P in equations M and N and get
From equation M, we have:
πΌ [
π1
πΏ
] =
π(π1πΏ)
ππ‘
+
π(πΏ2
)
ππ‘
But from equation P, we have
π
ππ‘
[(πΏ2)] = 0
So, we end with
πΌ [
π1
πΏ
] =
π(π1πΏ)
ππ‘
+ 0
Upon simplification, we have:
πΌ
πΏ
=
ππΏ
ππ‘
β¦ . π±
Similarly, from equation N, we have
πΌ [
π1
πΏ
] =
π(π1πΏ)
ππ‘
β
π(πΏ2
)
ππ‘
But from equation P, we have:
π
ππ‘
[(πΏ2)] = 0
So, we end with:
πΌ [
π1
πΏ
] =
π(π1πΏ)
ππ‘
β 0
We finally end with:
30. πΌ
πΏ
=
ππΏ
ππ‘
β¦ π²
We see that equation K and J are similar and so we solve for πΏ to get:
πΏ = β2πΌπ‘
We finally substitute in the temperature profile to get:
π β πβ
ππ β πβ
=
cosh (
π2 β π
πΏ
)
cosh (
π2 β π1
πΏ
)
OR
π β πβ
ππ β πβ
=
cosh (
π2 β π
β2πΌπ‘
)
cosh (
π2 β π1
β2πΌπ‘
)
32. CASE1: SEMI-INFINITE CASE
The governing equation is:
πΆ
ππ
π»
πππ
+ πΆ
π
π
ππ»
ππ
β
ππ·
π¨ππͺ
(π» β π»β) =
ππ»
ππ
π = 4ππ
π΄ = 2πππ
Where:
π = βπππβπ‘ ππ ππ¦ππππππ
Upon substituting the above in the heat equation, we get:
πΆ
ππ
π»
πππ
+ πΆ
π
π
ππ»
ππ
β
ππ
π ππͺ
(π» β π»β) =
ππ»
ππ
The boundary conditions are:
π = ππ ππ‘ π = π1
π = πβ ππ‘ π = π = β
The initial condition is:
π = πβ ππ‘ π‘ = 0
The temperature profile that satisfies the boundary conditions above is:
π β πβ
ππ β πβ
= π
β(πβπ1)
πΏ
33. πΌ
π2
π
ππ2
+ πΌ
1
π
ππ
ππ
β
2β
πππΆ
(π β πβ) =
ππ
ππ‘
We multiply through by r the heat equation as shown below and solve.
πΌπ
π2
π
ππ2
+ πΌ
ππ
ππ
β
2β
πππΆ
π(π β πβ) =
πππ
ππ‘
We transform the PDE into an integral equation and take the limits to be from
π = π1 to π = π = β
πΌ β« (π
π2
π
ππ2
)ππ
π
π1
+ πΌ β« [
ππ
ππ
]ππ
π
π1
β
2β
πππΆ
β« (π(π β πβ))ππ
π
π1
=
π
ππ‘
β« (ππ)ππ
π
π1
We evaluated those integrals before to be:
β« (π
π2
π
ππ2
) ππ
β
π1
=
(ππ β πβ)
πΏ
(π1 + πΏ)
β« [
ππ
ππ
]ππ
β
π1
= β(ππ β πβ)
2β
πππΆ
β« (π β πβ)ππ
π =β
π1
=
πΏβ
πππΆ
(ππ β πβ)
From the derivations above, we get:
β« (
π2
π
ππ2
) ππ
π
π1
=
(ππ β πβ)
πΏ
π
ππ‘
β« πππ
π
π1
=
ππΏ
ππ‘
(ππ β πβ)
β« (ππ)ππ
π =β
π1
= (ππ β πβ)(π1πΏ + πΏ2) + πβ(π β π1)
β« (π(π β πβ))ππ
π
π1
= (ππ β πβ)(π1πΏ + πΏ2
)
π
ππ‘
β« (π(π β πβ))ππ
π
π1
=
π
ππ‘
[(ππ β πβ)(π1πΏ + πΏ2
) + πβ(π β π1)]
But
π(πβ(π β π1))
ππ‘
= 0 π ππππ πβ πππ (π β π1) πππ ππππ π‘πππ‘π
34. So, we are left with
πΌ [
(ππ β πβ)
πΏ
(π1 + πΏ) β (ππ β πβ)] β (ππ β πβ)
2β
πππΆ
(π1πΏ + πΏ2) =
π
ππ‘
[(ππ β πβ)(π1πΏ + πΏ2)]
We are left with:
πΌ
π1
πΏ
β
2β
πππΆ
(π1πΏ + πΏ2) =
π
ππ‘
[(π1πΏ + πΏ2)]
Multiplying through by πΏ we get:
πΌπ1 β
2β
πππΆ
πΏ(π1πΏ + πΏ2) =
π
ππ‘
[πΏ(π1πΏ + πΏ2)]
Calling πΏ(π1πΏ + πΏ2) as X i.e.,
π = πΏ(π1πΏ + πΏ2)
We get:
πΌπ1 β
2β
πππΆ
π =
ππ
ππ‘
We solve the above 0DE with limits that at π‘ = 0 π = 0 since πΏ = 0 ππ‘ π‘ = 0
And we get:
π =
πΎππ1
2β
(1 β π
β2βπ‘
πππΆ )
Substituting for X we get:
πΏ(π1πΏ + πΏ2) =
πΎππ1
2β
(1 β π
β2βπ‘
πππΆ )
Upon simplifying we get:
πΉπ
+ πππΉπ
β
π²π ππ
ππ
(π β π
βπππ
π ππͺ ) = π
Which is a cubic function that can be solved to get πΏ as a function of time.
In steady state when time t tends to infinity, we get:
πΉπ
+ πππΉπ
β
π²π ππ
ππ
= π
35. CASE2: CONVECTION AT THE FREE END
The boundary and initial conditions are:
π» = π»π ππ π = ππ
βπ
π π»
π π
= πππ
(π» β π»β) ππ π = ππ
π» = π»β ππ π = π
This same analysis can be extended to a metal rod with convection at the other
end of the metal rod where the temperature profile is given by [1]:
π β πβ
ππ β πβ
=
cosh[π(π2 β π)] + (
βπ2
ππ
) sinh[π(π2 β π)]
cosh π(π2 β π1) + (
βπ2
ππ
) π ππβπ(π2 β π1)
Or
π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
] + (
βπ2
πΏ
π
) sinh[
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
To show that the initial condition is satisfied we assume from the above that
ππ‘ π‘ = 0, πΏ = 0.
π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
] + (
βπ2
πΏ
π
) sinh[
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
Becomes:
π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
=
π
(π2βπ)
πΏ + π
β(π2βπ)
πΏ
π
π2βπ1
πΏ + π
β(π2βπ1)
πΏ
π
β(π2βπ)
πΏ = πβ
(π2βπ)
0 = πββ(πΏβπ₯)
= 0
Similarly
π
β(π2βπ1)
πΏ = π
β(π2βπ1)
0 = πββ(π2βπ1)
= 0
36. So, we are left with
π β πβ
ππ β πβ
=
π
(π2βπ)
πΏ
π
π2βπ1
πΏ
= π
β(πβπ1)
πΏ = π
β(πβπ1)
0 = πββ(πβπ1)
= 0
Hence at π‘ = 0, π = πβ and hence the initial condition.
We use this temperature profile which satisfies the initial condition to solve the
heat equation and get πΏ as shown below:
Boundary and initial conditions are:
π» = π»π ππ π = ππ
βπ
π π»
π π
= πππ
(π» β π»β) ππ π = ππ
π» = π»β ππ π = π
The governing temperature profile is:
π β πβ
ππ β πβ
=
cosh [
(π2 β π)
πΏ
] + (
βπ2
πΏ
π
) sinh[
(π2 β π)
πΏ
]
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
Which we can express as:
π» β π»β = π¨ ππ¨π¬π‘ [
(ππ β π)
πΉ
] + ππ¬π’π§π‘ [
(ππ β π)
πΉ
]
Where:
π΄ =
(ππ β πβ)
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
And
π΅ =
(
βπ2
πΏ
π
)(ππ β πβ)
cosh
(π2 β π1)
πΏ
+ (
βπ2
πΏ
π
)π ππβ
(π2 β π1)
πΏ
The governing equation is
37. πΆ
ππ
π»
πππ
+ πΆ
π
π
ππ»
ππ
β
ππ·
π¨ππͺ
(π» β π»β) =
ππ»
ππ
Where:
π = 4ππ
π΄ = 2πππ
Upon substitution of the above in the heat equation, we get:
πΆ
ππ
π»
πππ
+ πΆ
π
π
ππ»
ππ
β
ππ
π ππͺ
(π» β π»β) =
ππ»
ππ
Multiplying through by r the heat equation becomes:
πΌπ
π2
π
ππ2
+ πΌ
ππ
ππ
β
2β
πππΆ
π(π β πβ) =
πππ
ππ‘
Transforming the PDE into an integral equation, we get:
πΌ [β« (π
π2
π
ππ2
) ππ
π2
π1
+ β« [
ππ
ππ
] ππ
π2
π1
] β
2β
πππΆ
β« (π(π β πβ))ππ
π2
π1
=
π
ππ‘
β« (ππ)ππ
π2
π1
Let us evaluate the integral
β« (π
π2
π
ππ2
)ππ
π2
π1
43. In steady state when time t tends to infinity, we get
πΏ = β
πΎπ
2β
And the temperature profile becomes:
π» β π»β
π»π β π»β
=
ππ¨π¬π‘
[
(ππ β π)
βπ²π
ππ ]
+
(
πππ
βπ²π
ππ
π
)
π¬π’π§π‘
[
(ππ β π)
βπ²π
ππ ]
ππ¨π¬π‘
(ππ β ππ)
βπ²π
ππ
+
(
πππ
βπ²π
ππ
π
)
ππππ
(ππ β ππ)
βπ²π
ππ
Again, we notice that the temperature profile above doesnβt reduce to the semi-
infinite temperature profile when π2 tends to infinity because both solutions
have different values of πΏ.
It can be shown that other transient boundary value problems where the
hollow cylinder is finite and not semi-infinite, the value of πΏ for lateral
convection case will be as derived above:
πΏ = β
πΎπ
2β
(1 β π
β4β
πππΆ
π‘
)
44. CONCLUSION
It should be noted that these equations are the ideal solutions of heat flow and
that experimental results are needed to verify the nature of some parameters
like the nature of the heat transfer coefficient at the end of the metal rod βπΏ.
Also, experimental results are needed to verify the transient nature of the heat
flow.
45. REFERENCES
[1] C.P.Kothandaraman, "Heat Transfer with Extendeded Surfaces(Fins)," in Fundamentals of Heat and
Mass Transfer, New Delhi, NEW AGE INTERNATIONAL PUBLISHERS, 2006, p. 129.
[2] C. E. W. R. E. W. G. L. R. James R. Welty, "HEAT TRANSFER FROM EXTENDED SURFACES," in
Fundamentals of Momentum, Heat, and Mass Transfer 5th Edition, Corvallis, Oregon, John Wiley &
Sons, Inc., 2000, pp. 236-237.