By S. Cho

2019-01-06 12:57:00 8 Comments

I'm working on the mathematical theory of parabolic equations. The prototype of such equations is heat equation given as follows : Let $\Omega$ be a bounded region of the space and $T>0$ a fixed time. In $\Omega_T=(0,T)\times \Omega$ we consider the following equation $$u_t =\alpha\Delta u -a(x)u,$$ $$u(0,x)=f(x),$$ where $f$ is the initial condition, $a$ a bounded potential, $\alpha>0$ is a constant, and $\Delta$ is the Laplacian. I'm wondering to know the physical meaning of the coefficient $a$ (and may be $\alpha$) and it's role in the heat process? Any reference or suggestion would be helpful.


@Alexander 2019-01-09 06:36:23

The proper physical name of your equation is diffusion equation with a source term. The equation can be rearranged to continuity equation - $u_t-\alpha u_{xx} = Q$. For $Q=0$ the time dependent solution can be shown to have time independent norm, which is manifestation of local mass conservation law. Source term means that particles can be created and destroyed locally, according to $Q(x)$ variation.
Continuity equation is a restatement of Gauss law - at given infinitesimal volume, the change in the number of particles in the volume is exactly equal to the number of particles crossed the surface of it in/out of this volume. You may gain some physical intuition exploring compressible aspect of the Navier-Stockes equation. The compressability is exactly the violation of continuity equation.

Closed form solution is given here. This wierd document seems related, however didn't find any peer reviewed articles.

@noisyoscillator 2019-01-08 05:47:12

The equation describes the flow of heat in presence of sources or sinks. The first term on the right hand side is the normal diffusion term. The second term can be thought of as a source or sink term. For more details see:

@N. Steinle 2019-01-06 13:24:23

The heat equation, as you've written it, models the flow of energy via thermal conduction (heat) through some region with well defined boundary conditions. You have yet to provide the specifics of the boundary region, so my answer will remain general and vague.

The $\alpha$ is the "diffusion coefficient" which is the isotropic form (diagonal terms only) of the diffusion tensor - alas the heat equation is a special case of the diffusion equation. So this coefficient tells us about how thermally diffuse the material that composes the region is (how diffusely distributed is the matter that the heat flows through?).

the physical meaning of the coefficient $a$

Sorry, at first I misread the equation (I thought it was merely a forcing term at first). And then secondly I mistook it for a convective term, but that's not correct since a convective term is typically proportional to $\frac{\partial u}{\partial x}$ (see equation 27 here). I have found that the term, $a(x)u$, could represent an approximative radiative term that is position dependent (for small radiative losses), i.e. see the last equation here. In which case, $a$ determines the strength of the radiation emitted from the conductor as a function of position. This radiation term is only meaningful for temperature variations in the rod that are small compared to the temperature of the surroundings, and in the case of larger fluctuations one must use a $u^4$ dependence instead (in accordance with Stefan-Boltzmann Law).

Here is a very nice write-up for non-homogeneous heat problems.

@Void 2019-01-06 13:27:54

The only note I would add is the fact that when you Wigner-rotate time $t\to i\tau$, you get the Schrödinger equation and $a(x)$ becomes the potential in which the particle is moving.

@N. Steinle 2019-01-06 13:30:13

@Void that's a very nice point, I'll add it to the answer if you may provide me with a source.

@S. Cho 2019-01-06 14:03:01

Thank you. I found in Wikipedia that the coefficient $a$ is a radiative coefficient which models radiative loss caused by low excess temperatures. Is that correct ?

@N. Steinle 2019-01-06 14:30:30

@S.Cho My pleasure! Which wiki article, specifically?

@Chester Miller 2019-01-06 14:44:22

In a heat transfer problem like this, the term involving a(x) is not a sink. It represents the convective transport of heat by fluid flow in the x direction.

@t t t t 2019-01-06 14:49:56

@S.Cho That's very strange. Radiative losses are usually of the form $u^4$. Unless you make the approximation that u does not vary appreciably, then I guess one can use a linear approximation...

@N. Steinle 2019-01-06 15:20:02

Interesting. Indeed it's not a sink. I don't think it's a convective term, since convective terms are typically proportional to $u_{x}$. I suspect it is a weak radiation term as @tttt suggests

@S. Cho 2019-01-06 16:10:03

@Steinle it's heat equation article in the section : the physical problem and the equation.

@S. Cho 2019-01-06 16:12:13

@t t t t Yes the form $a u^4$ is for height radiations and $a u$ for low radiations.

@Chester Miller 2019-01-06 18:08:05

Oops. You're right. I didn't notice that.

@Chemomechanics 2019-01-06 16:34:31

As discussed here under "Incorporating lateral heat transfer" (disclaimer: my site), if you're considering a 1-D transient heat transfer problem as suggested by the variables $x$ and $t$, then the equation $$k\Delta T(x,t)-h(x)T(x,t)=c\rho\dot T(x,t)$$

represents axial conduction with thermal conductivity $k$, linear lateral heat dissipation (through conduction, convection, and/or slight radiation) with spatially dependent coefficient $h(x)$, and energy storage with specific heat capacity $c$ and density $\rho$. $T(x,t)$ is the temperature excursion from some ambient value.

The qualification of "slight" radiation is to ensure linearity of $T(x,t)$ in that term. For convection, $h$ is simply a convection coefficient. As discussed in the link, $h$ might also represent lateral conduction to an adjacent temperature sink (for a suspended microfabricated beam, say).

If we change variables from $T(x,t)$ to $u$ and divide by $c\rho$, then we have

$$\alpha \Delta u-\left(\frac{h(x)}{c\rho}\right)u=u_t,$$

with $\alpha$ being the thermal diffusivity, which matches your equation and indicates that $a(x)$ corresponds to a spatially varying lateral heat coefficient divided by the specific heat capacity and the density. This is the physical interpretation of that parameter for this type of system (I solve the equation here).

@S. Cho 2019-01-07 11:28:56

Is it the same for the parameters appearing in the dynamic boundary conditions ? More precisely, if $\Gamma=\partial \Omega$ is the boundary of the domain, the dynamic boundary conditions on $\Gamma$ is $\partial_t y_\Gamma =\beta \Delta_\Gamma y_\Gamma +\alpha \partial_\nu y -b(x) y_\Gamma$, on $\Gamma$. I mean the parameters $\beta$ and $b$, ($\alpha$ is the same as the first equation).

@Chemomechanics 2019-01-07 19:16:33

What is $\partial_\nu$ in this case?

@S. Cho 2019-01-07 22:08:33

$\partial_\nu y = \nabla y \cdot \nu$ is the normal derivative of $y$ where $\nu$ is the unit outer normal vector on $\Gamma$.

@Chemomechanics 2019-01-08 18:31:02

This would seem to correspond to conduction within the system with thermal diffusivity $\beta$, lateral convective heat transfer to the environment as mediated by a coefficient $c\rho b(x)$, and lateral conductive heat transfer to the environment as mediated by a thermal conductivity $(-c\rho\alpha)$.

@Vincent Fraticelli 2019-01-06 13:13:58

In the study of the thermal transfer within a heat sink, we have a term of the form a * (T-Text) which correspond to the conducto convective exchanges between the heat sink and the air surrounding it: it is proportional to the temperature difference in accordance with Newton's law. The first term, in alpha, corresponds to the thermal conduction within the material. The thermal current density is proportional to the first spatial derivative of the temperature and the variation of this density leads to the second derivative (Laplacian). The alpha in the équation is the thermal diffusivity (conductivity/mu*C)

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