Give step-by-step explanation and final answer Consider a slab with thickness
"
a
"
a
t
a
n
initial temperature
T
θ
.
One face
o
f
this slab
i
s
contacted with
a
coolant
o
f
temperature
T
I
.
A
t
this surface heat
i
s
transferred
t
o
the coolant convectively obeying
Newton's law
o
f
cooling with a heat transfer coefficient
h
.
Temperature
o
f
the other face
i
s
kept constant
a
t
T
θ
.
Calculate the unsteady state temperature profile
T
=
T
(
x
,
t
)
.
IMPORTAT!!!! : Use separation
o
f
variables technique.
Question:
Give step-by-step explanation and final answer Consider a slab with thickness
"
a
"
a
t
a
n
initial temperature
T
θ
.
One face
o
f
this slab
i
s
contacted with
a
coolant
o
f
temperature
T
I
.
A
t
this surface heat
i
s
transferred
t
o
the coolant convectively obeying
Newton's law
o
f
cooling with a heat transfer coefficient
h
.
Temperature
o
f
the other face
i
s
kept constant
a
t
T
θ
.
Calculate the unsteady state temperature profile
T
=
T
(
x
,
t
)
.
IMPORTAT!!!! : Use separation
o
f
variables technique.
This is AI generated Response.
Asked by: Test User 100192
Created at: 2025-05-18 13:56:32
Final Answer:
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Let's break this down step by step.
## **Given:**
- Slab thickness = \( a \)
- Initial temperature = \( T_\theta \)
- One face at \( x=0 \) is **convectively cooled** by fluid at \( T_\infty \), heat transfer coefficient \( h \)
- Other face at \( x=a \) is kept at constant temperature \( T_\theta \)
- \( T(x, t) \) is the temperature profile to be found.
- **Use separation of variables.**
---
## **1. Governing Equation**
For 1D heat conduction (no internal heat generation):
\[
\frac{\partial T}{\partial t} = \alpha \frac{\partial^2 T}{\partial x^2}
\]
where \(\alpha\) = thermal diffusivity.
---
## **2. Initial and Boundary Conditions**
- **Initial condition:**
\[
T(x, 0) = T_\theta, \quad 0 \leq x \leq a
\]
- **Boundary conditions:**
1. At \( x = 0 \): Convective boundary
\[
-k \left. \frac{\partial T}{\partial x} \right|_{x=0} = h [T(0, t) - T_\infty]
\]
2. At \( x = a \): Dirichlet (fixed temperature)
\[
T(a, t) = T_\theta
\]
---
## **3. Non-dimensionalization (for simplification)**
Let us define the dimensionless temperature:
\[
\theta(x, t) = \frac{T(x, t) - T_\infty}{T_\theta - T_\infty}
\]
So, the conditions become:
- \(\theta(x, 0) = 1\)
- \(\theta(a, t) = 1\)
- At \(x=0\): \( -k \frac{\partial \theta}{\partial x} = h (T_\theta - T_\infty) [\theta(0, t)] \implies -k \frac{\partial \theta}{\partial x} = h (T_\theta - T_\infty) \theta(0, t)\)
- Or, dividing both sides by \(k (T_\theta - T_\infty)\):
\[
-\left. \frac{\partial \theta}{\partial x} \right|_{x=0} = \frac{h}{k} \theta(0, t)
\]
Let \( Bi = \frac{h a}{k} \) (Biot number), and rescale \( x \) by \( a \): \( \xi = \frac{x}{a} \), \( 0 \leq \xi \leq 1 \).
So, the PDE becomes:
\[
\frac{\partial \theta}{\partial t} = \alpha \frac{\partial^2 \theta}{\partial x^2}
\]
with
- \( \theta(x, 0) = 1 \)
- \( \theta(a, t) = 1 \)
- \( -\frac{\partial \theta}{\partial x}|_{x=0} = \frac{h}{k} \theta(0, t) \)
---
## **4. Separation of Variables**
Let \( \theta(x, t) = X(x) \cdot T(t) \).
Plug into the PDE:
\[
X(x) \frac{dT}{dt} = \alpha T(t) \frac{d^2 X}{dx^2}
\]
\[
\Rightarrow \frac{1}{\alpha T(t)} \frac{dT}{dt} = \frac{1}{X(x)} \frac{d^2 X}{dx^2} = -\lambda^2
\]
So:
- \( \frac{dT}{dt} + \alpha \lambda^2 T = 0 \implies T(t) = A e^{-\alpha \lambda^2 t} \)
- \( \frac{d^2 X}{dx^2} + \lambda^2 X = 0 \implies X(x) = B \cos(\lambda x) + C \sin(\lambda x) \)
---
## **5. Apply Boundary Conditions to \(X(x)\)**
**At \( x = a \):**
\[
X(a) = 0 \implies B \cos(\lambda a) + C \sin(\lambda a) = 0
\implies B \cos(\lambda a) = -C \sin(\lambda a)
\]
**At \( x = 0 \):**
\[
-k \frac{dX}{dx}\bigg|_{x=0} = h X(0)
\]
\[
\frac{dX}{dx} = -B \lambda \sin(\lambda x) + C \lambda \cos(\lambda x)
\]
At \(x=0\):
\[
\frac{dX}{dx}|_{x=0} = C \lambda
\]
So:
\[
-k C \lambda = h B
\]
Or:
\[
C \lambda = -\frac{h}{k} B
\implies C = -\frac{h}{k \lambda} B
\]
---
Now plug this for \(C\) into the expression from the Dirichlet BC at \(x=a\):
\[
B \cos(\lambda a) + C \sin(\lambda a) = 0
\]
\[
B \cos(\lambda a) - \frac{h}{k \lambda} B \sin(\lambda a) = 0
\]
\[
\cos(\lambda a) - \frac{h}{k \lambda} \sin(\lambda a) = 0
\]
\[
\frac{h}{k \lambda} \sin(\lambda a) = \cos(\lambda a)
\]
\[
\frac{\sin(\lambda a)}{\cos(\lambda a)} = \frac{k \lambda}{h}
\]
\[
\tan(\lambda a) = \frac{k \lambda}{h} = \frac{\lambda a}{Bi}
\]
So, the **eigenvalue equation** is:
\[
\tan(\lambda_n a) = \frac{\lambda_n a}{Bi}
\]
where \( Bi = \frac{h a}{k} \).
---
## **6. General Solution**
Given the eigenvalues \( \lambda_n \) (solutions of the transcendental equation above), the general solution is:
\[
\theta(x, t) = \sum_{n=1}^{\infty} A_n X_n(x) e^{-\alpha \lambda_n^2 t}
\]
with
\[
X_n(x) = \cos(\lambda_n x) - \frac{h}{k \lambda_n} \sin(\lambda_n x)
\]
or, factoring \(B\) (which can be absorbed into \(A_n\)):
\[
X_n(x) = \cos(\lambda_n x) - \frac{Bi}{\lambda_n a} \sin(\lambda_n x)
\]
---
## **7. Determine Coefficients \(A_n\)**
From the initial condition:
\[
\theta(x, 0) = 1 = \sum_{n=1}^{\infty} A_n X_n(x)
\]
The coefficients \(A_n\) can be found by using the orthogonality of the eigenfunctions (see standard methods for Sturm-Liouville problems). For such mixed boundary conditions, the eigenfunctions are orthogonal with weight 1.
So:
\[
A_n = \frac{ \int_{0}^{a} 1 \cdot X_n(x) dx }{ \int_{0}^{a} X_n^2(x) dx }
\]
---
## **8. Final Answer**
\[
\boxed{
T(x, t) = T_\infty + (T_\theta - T_\infty) \sum_{n=1}^{\infty} A_n \left[ \cos(\lambda_n x) - \frac{Bi}{\lambda_n a} \sin(\lambda_n x) \right] e^{-\alpha \lambda_n^2 t}
}
\]
Where:
- \( \lambda_n \) are the positive roots of \( \tan(\lambda_n a) = \frac{\lambda_n a}{Bi} \)
- \( Bi = \frac{h a}{k} \)
- \( A_n = \frac{ \int_0^a X_n(x) dx }{ \int_0^a [X_n(x)]^2 dx } \)
- \( X_n(x) = \cos(\lambda_n x) - \frac{Bi}{\lambda_n a} \sin(\lambda_n x) \)
---
### **Summary Table**
| Step | Description | Equation(s) |
|------|-------------|-------------|
| 1 | Heat eqn | \( \frac{\partial T}{\partial t} = \alpha \frac{\partial^2 T}{\partial x^2} \) |
| 2 | IC | \( T(x,0) = T_\theta \) |
| 3 | BC at \( x=0 \) | \( -k \frac{\partial T}{\partial x} = h(T - T_\infty) \) |
| 4 | BC at \( x=a \) | \( T(a, t) = T_\theta \) |
| 5 | Eigenvalue eqn | \( \tan(\lambda_n a) = \frac{\lambda_n a}{Bi} \) |
| 6 | General soln | See boxed formula above |
| 7 | Coefficient | \( A_n = \frac{ \int_0^a X_n(x) dx }{ \int_0^a [X_n(x)]^2 dx } \) |
---
### **References**
- Carslaw and Jaeger, "Conduction of Heat in Solids" (Section 3.3)
- Incropera & DeWitt, "Fundamentals of Heat and Mass Transfer" (Transient Conduction)
---
**If you need help evaluating \(A_n\) or want a more explicit form, let me know!**
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