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Conductive Heat Transfer
Initial and boundary conditions
 
 
Conductive Heat Transfer

The equation for the conductive heat transfer in a continuous medium can be derived by imposing the principle of heat energy conservation over an arbitrary fixed volume (V) of the medium, which is bounded by a closed surface (S) [Lew96], [Red94]. For convenience, the energy conservation principle is expressed in a rate formula and given by

If u denotes specific internal energy of the medium, then the left side of Eq. (2.1) yields
where is the density of a medium. By introducing the specific heat(cp) of the medium defined by
where T is the temperature. Equation (2.2) can be rewritten as
To obtain an expression for the rate formula of heat conduction into Vacross S, the Fourier law of the heat conduction is introduced. This is an empirical relationship saying that, for a surface with a unit normal vector , the rate at which heat is conducted across the surface, per unit area, in the direction of , is given by
where k is a property of the medium termed the thermal conductivity . In this Eq. (2.5), denotes differentiation in the direction of and q is termed the heat flux in this direction. Thus, it follows that
where the Divergence theorem has been applied. If it is assumed that heat generation in the medium is occurring at a rate Qper unit volume, then
Combining Eq. (2.4), (2.6) and (2.7) into (2.1) produces an energy conservation statement as follows
and, since the volume V was arbitrarily chosen initially, it follows that
everywhere in the medium. This is the familiar formula for the heat conduction equation in a non-stationary system. If the medium is anisotropic, i.e., if the conductivity depends upon the direction, the formula of the heat conduction equation is modified, yielding
where is the conductivity tensor and, for example, kxy denotes the thermal conductivity in the xdirection across the surface with a normal in the y direction.
If the conductivity k and the specific heat capacity are assumed to be constant and if the heat generation rate Q is independent of temperature T, Eq. (2.9) will become a linear function. Recall that the linearized heat conduction equation is represented by
where is termed a thermal diffusivity of the medium and denotes the Laplacian operator defined in Cartesian coordinates as follows
Without heat generation within the medium, Eq. (2.11) reduces to the standard diffusion equation ,
If the temperature does not vary with time, a steady-state condition is said to exist. Here the governing equation simplifies the Laplace equation further as follows
Initial and boundary conditions
Suppose that the solution of Eq. (2.9) is required over an arbitrary domain bounded by a closed surface , as illustrated in Fig. 2.1.
Figure 2.1: General domain and boundary for the heat transfer equation.
If the problem being modeled is independent of time, the solution will be uniquely defined with appropriate boundary conditions . For the heat conduction equation in steady state , one condition should be specified at each point of the boundary curve . In general, the boundary conditions can be classified into two types, given by:
1. Dirichlet or essential boundary conditions
This is in the situation when the temperature distribution is prescribed at the boundary surface , which is
This is known as the dirichlet boundary condition or essential boundary condition .
2. Neumann or natural boundary conditions
Here the value of the outward normal heat flux is given by
This boundary condition is also known as the neumann boundary condition or natural
This boundary condition is also known as the neumann boundary condition or natural boundary condition . Here f, , and are prescribed functions of and T, and , . In Eq. (2.16), denotes a convective heat flux , defined as follows
where h is a coefficient of surface heat transfer and is a specified ambient temperature of the surrounding medium. The is a radiative heat flux that is
where is the Stefan-Boltzmann constant and is an emissivity of the surface. Here, the emissivity is defined as the ratio of the heat emitted by a surface to the heat emitted by a black body at the same temperature.
As was shown above, the heat transfer problem is a branch of engineering applications that deals with the transfer of thermal energy; the thermal energy moves from one point to another within the medium or from one medium to another due to the temperature difference. Therefore, heat transfer may be take place in one or more of three basic forms: conduction, convection, and radiation.
Conduction:
Conductive heat transfer exists in any material whether solid, gas, or liquid. This phenomenon is driven by a temperature gradient within the material and is dependent on the thermal conductivity of the material. In a typical electronics problem, this value can range from 400W/mK for copper to 0.0261W/mK for air - several orders of magnitude difference. The conductivity may vary locally with parameters such as local temperature especially in silicon. It may not be isotropic particularly for circuit boards, where the copper layers play a critical part in the heat spreading.
Convection:
Convective heat transfer is defined as energy transport by a moving fluid such as liquid or gas. The convective heat-transfer efficiency from the solid to the fluid depends on the fluid velocity over the source and the convection regime. This regime can be characterized as laminar (low speed) where the streamlines follow a kind of parallel pattern, or turbulent (high speed). In the latter case, a strong mixture occurs between the streamlines enhancing the heat transfer ultimately. Convection is the critical part of design problems in electronic systems. It is usually characterized as either:
Forced convection occurs when air/fluid movers (fans or pumps) are used to create the flow.
Natural convection is the flow created by a variation of the fluid density with temperature (buoyancy ).
Radiation:
Radiative heat transfer is defined as radiant energy emitted by a medium and is due solely to the temperature of a medium. Radiant energy exchange between surfaces or between a region and its surrounding is described by the Stefan-Boltzmann law . It says that the radiant energy transmitted is proportional to the difference of the fourth power of the surface temperatures. Unlike the conduction and convection, the radiation does not require a conductive medium to take place. Consequently, heat transfer by the radiation is potentially present everywhere. The radiation is a major heat transfer mechanism for space applications but is generally negligible in forced convection systems. However, many of the applications such as laptop computers, cellular telephones, PDA's and telecom's exchange equipment use natural convection cooling. Frequently, these enclosures are partially, if not completely, sealed and the radiation is no longer negligible when compared to the convection. When the heat transfer problem being modeled is time dependent (transient state) , the solution is uniquely defined with an initial condition and a boundary condition at each point of the boundary . The initial condition should give the distribution of temperature over the entire domain of at the initial time, usually taken to be time t=0. Furthermore, the function f, ,.
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