ME 353 Heat Transfer 1
M.M. Yovanovich
CONDEQ1.MWS
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Derivation of Conduction Equation in Cartesian Coordinates.
The solid has volumetric heat sources which are the result
of a variety of processes such as chemical, electrical, nuclear,
biological, mechanical, etc.
Assume that the properties are constant.
Obtain the following special cases from the general
three-dimensional equation:
1) Two-dimensional transient without heat sources: T(x, y, t) and P = 0;
2) One-dimensional transient with heat sources: T(x, t) and P > 0;
3) Two-dimensional, steady-state with sources: T(x, y) and P > 0;
4) Two-dimensional, steady-state without sources: T(x, y) and P = 0;
5) One-dimensional, steady-state with heat sources: T(x) and P > 0;
6) One-dimensional, steady-state without heat souces: T(x) and P = 0.
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> restart:
Conduction rates into the control volume dV = dx dy dz.
> Q[x]:= - k*dA[x]*diff(T(x, y, z, t), x);
> Q[y]:= - k*dA[y]*diff(T(x, y, z, t), y);
> Q[z]:= - k*dA[z]*diff(T(x, y, z, t), z);
Conduction rates out of the control volume dV = dx dy dz. The first two terms of the Taylor series expansion are taken.
> Q[x + dx]:= Q[x] + diff(Q[x], x)*dx;
> Q[y + dy]:= Q[y] + diff(Q[y], y)*dy;
> Q[z + dz]:= Q[z] + diff(Q[z], z)*dz;
Define the differential conduction areas.
>
dA[x]:= dy*dz;
>
dA[y]:= dx*dz;
>
dA[z]:= dx*dy;
Net heat conduction rate into the differential control volume through the six
faces.
>
Q[cond_net]:=
Q[x] + Q[y] + Q[z] - Q[x + dx]
- Q[y + dy] - Q[z + dz];
Heat generation rate within the differential control volume due to distributed
volumetric heat sources. P is the volumetric heat source strength. P is the volumetric heat source strength.
Units are W/m^3.
>
Q[gen]:= P*dV;
Rate of energy storage within the differential control volume.
>
Q[storage]:=
rho*c[p]*diff(T(x, y, z, t), t)*dV;
> dV:= dx*dy*dz;
By means of an energy balance over the differential control
volume obtain the general three-dimensional conduction equation.
Divide by k*dV and simplify.
>
eq:=
expand((Q[cond_net] - Q[gen] =
Q[storage])/(k*dV));
Introduce the thermal diffusivity alpha = k/(rho*cp) into the equation.
> eq:= subs(rho = k/alpha/c[p], eq);
The above equation is the three-dimensional diffusion equation
within a substance that has distributed volumetric heat sources.
The properties are assumed to be constant.
This partial differential equation is second-order in space and
first order in time.
It therefore requires one initial condition and six boundary
conditions to obtain its solution.
The above general equation can be used to obtain special cases.
A few special cases will be obtained below.
1) Two-dimensional transient without heat sources:
T(x, y, t) and P = 0;
>
DiffusionEq_2D:=
expand(
subs(T(x, y, z, t) = T(x, y, t), P = 0, eq));
2) One-dimensional transient with heat sources: T(x, t) and P > 0;
>
DiffusionPoissonEq_1D:=
expand(
subs(T(x, y, z, t) = T(x, t), eq));
3) Two-dimensional, steady-state with sources: T(x, y) and P > 0;
>
DiffusionPoissonEq_2D:=
expand(
subs(T(x, y, z, t) = T(x, y, t), eq));
4) Two-dimensional, steady-state without sources: T(x, y) and P = 0;
>
LaplaceEq_2D:=
expand(
subs(T(x, y, z, t) = T(x, y), P = 0, eq));
5) One-dimensional, steady-state with heat sources: T(x) and P > 0;
>
PoissonEq_1D:=
expand(
subs(T(x, y, z, t) = T(x), eq));
6) One-dimensional, steady-state without heat souces: T(x) and P = 0.
>
LaplaceEq_1D:=
expand(
subs(T(x, y, z, t) = T(x), P = 0, eq));
>