Heat equation
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The heat equation or diffusion equation is an important partial differential equation which describes the variation of temperature in a given region over time. In the special case of heat propagation in an isotropic and homogeneous medium in the 3-dimensional space, this equation is
- <math>u_t = k ( u_{xx} + u_{yy} + u_{zz} ) \quad <math>
where:
- u(t, x, y, z) is temperature as a function of time and space;
- ut is the rate of change of temperature at a point over time;
- <math>u_{xx}<math>, <math>u_{yy}<math>, and <math>u_{zz}<math> are the second spatial derivatives (thermal conductions) of temperature in the x, y, and z directions, respectively
- k is a material-specific constant (thermal diffusivity)
To solve the heat equation, we also need to specify boundary conditions for u.
Solutions of the heat equation are characterized by a gradual smoothing of the initial temperature distribution by the flow of heat from warmer to colder areas of an object.
The heat equation is the prototypical example of a parabolic partial differential equation.
Using the Laplace operator, the heat equation can be generalized to
- <math>u_t = k \Delta u \quad <math>
Heat conduction in non-homogeneous anisotropic media
In general, the study of heat conduction is based on several principles. Heat flow is a form of energy flow, and as such it is meaningful to speak of the time rate of flow of heat into a region of space.
- The time rate of heat flow into a region V is given by a time-dependent quantity qt(V). We assume q has a density, so that
- <math> q_t(V) = \int_V Q(t,x)\,d x \quad <math>
- Heat flow is a time-dependent vector function H(x) characterized as follows: the time rate of heat flowing through an infinitesimal surface element with area d S and with unit normal vector n is
- <math> \mathbf{H}(x) \cdot \mathbf{n}(x) \, dS <math>
Thus the rate of heat flow into V is also given by the surface integral
- <math> q_t(V)= - \int_{\partial V} \mathbf{H}(x) \cdot \mathbf{n}(x) \, dS <math>
where n(x) is the outward pointing normal vector at x.
- The Fourier law states that heat energy flow has the following linear dependence on the temperature gradient
- <math> \mathbf{H}(x) = -\mathbf{A}(x) \cdot [\operatorname{grad}(u)] (x) <math>
- where A(x) is a 3 × 3 real matrix, which in fact is symmetric and non-negative.
By Green's theorem, the previous surface integral for heat flow into V can be transformed into the volume integral
- <math> q_t(V) = - \int_{\partial V} \mathbf{H}(x) \cdot \mathbf{n}(x) \, dS <math>
- <math> = \int_{\partial V} \mathbf{A}(x) \cdot [\operatorname{grad}(u)] (x) \cdot \mathbf{n}(x) \, dS <math>
- <math> = \int_V \sum_{i, j} \partial_{x_i} a_{i j} \partial_{x_j} u (t,x)\,dx <math>
- The time rate of temperature change at x is proportional to the heat flowing into an infinitesimal volume element, where the constant of proportionality is dependent on a constant κ
- <math> \partial_t u(t,x) = \kappa(x) Q(t,x)\, dx<math>
Putting these equations together gives the general equation of heat flow:
- <math> \partial_t u(t,x) = \kappa(x) \sum_{i, j} \partial_{x_i} a_{i j} \partial_{x_j} u (t,x) <math>
Remarks.
- The constant κ(x) is the inverse of specific heat of the substance at x × density of the substance at x.
- In the case of an isotropic medium, the matrix A is a scalar matrix equal to thermal conductivity.
- The Jacobi theta function is the unique solution to the one-dimensional heat equation with periodic boundary conditions at t = 0.
External links
- Derivation of the heat equation (http://www.mathphysics.com/pde/HEderiv.html)
- Linear heat equations (http://eqworld.ipmnet.ru/en/solutions/lpde/heat-toc.pdf): Particular solutions and boundary value problems - from EqWorld
- Nonlinear heat equations (http://eqworld.ipmnet.ru/en/solutions/npde/npde-toc1.pdf): Exact solutions - from EqWorld
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