# Custom Equations and the Weak PDE Formulation Equation Syntax

The following post further examines PDE equation parsing and specifying custom equations in FEATool. Furthermore, a simple parametric heat transfer model will be shown and set up as a custom PDE equation, suitable for both the MATLAB command line and m-script file modeling.

Stationary heat transfer by conduction and convection is modeled by the following PDE

\[ \nabla\cdot(-k\nabla T + \rho C_p\mathbf{u}T) = Q \]

where $\rho$ is the density, $C_p$ the heat capacity, $k$ is the thermal conductivity, $Q$ heat source term, and $\mathbf{u}$ a vector valued convective velocity field.

In the FEATool custom PDE equation syntax this equation can in one dimension be written as

```
-k*Tx_x + rho*Cp*u*T_x = Q
```

Note that each term may only contain one underscore to indicate that it is a bilinear form to be assembled, meaning that the term is multiplied with a test function to which partial integration is applied as in the usual finite element formulation. The term will then contribute to the implicit FEM system and stiffness matrix. In contrast, this equation looks almost identical

```
-k*Tx_x + rho*Cp*u*Tx = Q
```

however, the convective 2nd term, does not feature an underscore and will thus be assembled as a linear term contribution to the right hand side (the force and load vector). The following equivalent equation will thus be solved instead

```
-k*Tx_x = Q - rho*Cp*u*Tx
```

If the velocity field is constant or divergence free, these two
conservative and non-conservative approaches both lead to the same
identical solution, although the latter approach will require a
non-linear solver since the right hand side depends on the unknown
solution *Tx*, in this case the first derivative. Also the natural
flux (Neumann) boundary conditions will look a little different since
they arise from partial integration of the bilinear terms (with the
underscores).

To see exactly what resulting weak form contributions results from a
custom equation one can use the
`parseeqn`

function in the MATLAB
workspace. For example

```
eqn = parseeqn( '-k*Tx_x + rho*Cp*u*T_x = Q' , {'T'}, {'x'} )
```

will result in the following fields (ignoring *eqn.m* which specifies
the mass matrix for time dependent problems)

```
>> eqn.a.form{:}
2 1
2 2
>> eqn.a.coef{:}
'k' '-rho*Cp*u'
```

The first row in the *form* equation field specifies trial functions
to use for the terms (1=function value, 2=x-derivative,
3=y-derivative, 4=z-derivative), and the bottom row the test
functions. Thus in *eqn.a* a bilinear form is specified which here
contains two terms the first $T_x\cdot v_x$ with coefficient *k*,
where $v$ is the finite element test function, and the second
$T\cdot v_x$ with coefficient *-rho*Cp*u*. Similarly, inspecting the
right hand side *f* field, we have

```
>> eqn.f.form{:}
1
>> eqn.f.coef{:}
'Q'
```

Compare that with the second non-conservative PDE formulation which
instead will result in one term for the bilinear form in *eqn.a* but
two linear forms in *eqn.f*

Let’s build a simple heat transfer model with the FEM weak form. First
we define a finite element ‘fea’ struct and name the 1D space
dimension to *x*, we also need a grid, in this case a line from *0* to
*1* with *100* grid cells

```
fea.sdim = { 'x' };
fea.grid = linegrid( 100, 0, 1 );
```

Furthermore, we name out dependent variable or unknown to *T* for
temperature and use 1st order linear Lagrange FEM shape functions to
approximate the solution

```
fea.dvar = { 'T' };
fea.sfun = { 'sflag1' };
```

Now we define the equations in the *fea.eqn* field as described
above. The equation coefficient and expressions are specified in a cell
array in the *fea.coef* or *fea.expr* fields

```
fea.eqn = parseeqn( '-k*Tx_x + rho*Cp*u*T_x = Q', ...
fea.dvar, fea.sdim );
fea.coef = { 'k', '1e-3 + 0.01*(x>0.5)' ;
'rho', 1 ;
'Cp' 1 ;
'u' 0 ;
'Q' 1 };
```

Note, that to make it more interesting we have defined a discontinuous
thermal conductivity `k = 1e-3 + 0.01*(x>0.5)`

that will
take on the value *1e-3* in the first half of the domain (x<0.5) and
*1e-3 + 0.01 = 0.011* in the second half.

Fixed value (Dirichlet) and flux (Neumann) boundary conditions are
defined in the *fea.bdr.d* and *fea.bdr.n* fields, respectively. In
this case we fix the temperature to *50* and *60* degrees at the two
end points.

```
fea.bdr.d = { 50 60 };
fea.bdr.n = { [] [] };
```

Finally, the following small script solves and plots the solution for
a number of different velocity *u* values.

```
figure, hold on
uvals = { '0' '0.01' '0.02' '0.03' '0.05' '0.1' };
colors = { 'r' 'g' 'b' 'c' 'm' 'y' };
for i=1:numel(uvals)
fea.coef{4,2} = uvals{i};
fea = parseprob( fea );
fea.sol.u = solvestat( fea );
postplot( fea, 'surfexpr', 'T', 'color', colors{i} )
[umax,j] = max( fea.sol.u );
text( fea.grid.p(j), umax, ['u = ',uvals{i}] )
end
ylabel( fea.dvar{1} )
xlabel( fea.sdim{1} )
axis( [0 1 50 100] )
axis normal
grid on
```

Resulting in the following parametric solutions for the temperature distribution.

**Category:**
heat transfer
pde