Heat Eq. (2)
last time:
- \( u(0, t) = 0 \)
- left temp = 0
- \( u(L, t) = 0 \)
- right temp = 0
- \( u(x, 0) = f(x) \)
- initial temp. profile
last time:
Copper plate/slab thickness 4 cm
\( k = 1.15 \text{ cm}^2/s \)
“core sample”
heat the entire interior uniformly to \( 100^\circ\text{C} \) at \( t = 0 \)
keep right and left faces at \( 0^\circ\text{C} \) for all \( t \)
Entire plate is uniformly heated and made of same material (same \( k \))
initial: \( f(x) = 100 \)
as \( t \to \infty \), the time solution \( \to 0 \) \( \to \) heat flows out of rod through ends
space solution \( \to \) periodic \( \to \) same temps on ends
what is the temp at the mid point \( (x=2) \) 3 seconds later \( (t=3) \)
in practice, the negative exponential makes this a fast converging series \( \to \) only few terms needed to get "good" approx.
1-term approx \( (n=1 \text{ only}) \to 15.16^{\circ}\text{C} \)
The graph illustrates the spatial distribution of temperature \(u\) along a one-dimensional domain \(x \in [0, 4]\) for several discrete time steps.
This graph depicts the temporal evolution of temperature at specific fixed points in space.
Two such slabs put together (\(4\text{ cm}\) thick each)
Two outer faces at \(0^\circ\text{C}\)
Left slab heated to \(50^\circ\text{C}\) at \(t=0\)
Right slab heated to \(100^\circ\text{C}\) at \(t=0\)
Initial temp:
\[ f(x) = \begin{cases} 50 & 0 < x < 4 \\ 100 & 4 < x < 8 \end{cases} \]
\(\vdots\)
The plot visualizes the heat diffusion over time in the composite slab system. The initial temperature discontinuity at \(x=4\) quickly smooths out as heat flows toward the cooler boundaries at \(x=0\) and \(x=8\).
The following graph illustrates the spatial temperature distribution \( u(x, t) \) across a rod of length \( L = 8 \) with a thermal diffusivity constant \( k = 1.15 \). The initial condition at \( t = 0 \) is a step function, which smooths out over time as heat diffuses through the medium.
This graph depicts the temporal evolution of temperature \( u(x, t) \) at specific fixed positions \( x \) along the rod. It demonstrates how the temperature at different points converges as time progresses.
now let's relax the ends at \( 0^{\circ}C \) constraint
\[ u_t = k u_{xx} \quad 0 < x < L \quad t > 0 \]
\[ u(0, t) = T_1 \]
\[ u(L, t) = T_2 \]
if \( T_1, T_2 \) are not zero, the BC's are nonhomogeneous
\[ u_{xx} = 0 \rightarrow u = C_1 + C_2 x \text{ using } u(0) = T_1, u(L) = T_2 \]
we get
\[ u = \frac{T_2 - T_1}{L} x + T_1 = v(x) \quad \text{steady-state temp.} \]
but what about the transient solution (when time still matters)
\[ u_t = k u_{xx} \]
\[ u(0, t) = T_1 \]
\[ u(L, t) = T_2 \]
\[ u(x, 0) = f(x) \]
\[ v(x) = \frac{T_2 - T_1}{L} x + T_1 \]
\[ w_t = u_t \quad w_{xx} = u_{xx} \rightarrow w_t = k w_{xx} \]
same heat eq.
\[ w(0, t) = 0 \]
\[ w(L, t) = 0 \]
\( \leftarrow \) BC's are homogeneous in \( w \)
solution is known
\[ w(x, t) = \sum_{n=1}^{\infty} B_n e^{-k n^2 \pi^2 t / L^2} \sin\left(\frac{n \pi x}{L}\right) \]
initial condition: \( u(x,0) = f(x) \)