Featuring an easy to use graphical user interface (GUI), *FEATool
Multiphysics* is also fully compatible with MATLAB functions and its
scripting language. As simulation models both can be saved in a binary
format and also as m-script language files, FEATool can therefore be
used with all built-in MATLAB functionality as well as with Simulink
and the Optimization Mathworks toolboxes.

Closely related to the article on parameter search and optimization in FEA
physics simulations
using the *fzero* MATLAB function, the following post illustrates how to
integrate and use the
*fminbnd*
minimization function with a finite element FEA simulation model to
conduct a quick and simple parameter search.

The example CFD problem used in the following considers two-dimensional potential flow around a solid object with the stream-function formulation, that is

*Δψ = 0*

where the velocities are defined as *u = -∂ψ/∂y* and *v
= ∂ψ/∂x*. Appropriate boundary conditions include
prescribed stream-function or free stream velocity on the external
boundary, and a prescribed constant stream-function value on the
body. If both the flow field and body shape are symmetric then the
value of the stream-function is zero on the body. However, for
non-symmetric flows and bodies the stream-function should be non-zero
in order to correct for non-physical flow field effects.

The issue is that at the sharp trailing edge of an airfoil or wing profile the velocity should be either zero or continuous in the normal direction of the flow field according to the Kutta condition. This can be achieved by offsetting the stream-function on the boundary of the airfoil. This phenomena is illustrated in the figure below.

In the left side simulation the flow field curls around the trailing edge and features an unphysical stagnation point on the top of the airfoil. In contrast, the results of the corrected right hand side simulation show a continuous flow field and streamlines from the trailing edge.

Although ineffective, one can use trial and error to find the actual
value and corrected value of the stream-function at the boundary of
the body. A better approach is to recognize that what we actually are
looking for, is to find the stream-function value on the body for
which the velocity at the trailing edge is zero or minimized. As the
magnitude of the velocity *U = √(u ^{2}+v^{2})*
will always be positive (and possibly not even numerically zero), the

*fzero*function can not be used. Instead the

*fminbnd*and potentially also

*fminsearch*MATLAB functions are appropriate here, and works in the same way as

*fzero*.

Define a MATLAB function that takes a one parameter argument, in this case the steam-function at the body, and returns the velocity magnitude at the trailing edge. The problem function in this example is defined as an anonymous function, but could just as well be implemented as a regular MATLAB function.

```
pfun = @(psi_body) velocity_at_trailing_edge(psi_body);
```

This function which constructs and solves the potential flow problem
is then called by *fminbnd* with lower and upper limits on *psi*

```
found_psi_body = fminbnd( pfun, psi_min, psi_max );
```

Running the script for a *NACA 0012* wing profile at a 6 degree angle
of attack, we find that *fminbnd* takes 11 tries in the search and
successfully narrows down the stream-function value to *-0.178*
yielding a minimum velocity magnitude at the trailing edge of
*0.78234*.

```
>> ex_potential_flow1
Func-count x f(x) Procedure
1 -2.36068 23.541 initial
2 2.36068 27.3679 golden
3 -5.27864 54.9821 golden
4 -0.267231 1.24343 parabolic
5 -0.0929204 1.20285 parabolic
6 -0.154739 0.821156 parabolic
7 -0.178032 0.783252 parabolic
8 -0.181615 0.78442 parabolic
9 -0.177581 0.78324 parabolic
10 -0.177624 0.78324 parabolic
11 -0.177658 0.78324 parabolic
Optimization terminated:
the current x satisfies the termination criteria using OPTIONS.TolX of 1.000000e-04
```

As shown in the figure below, the solution and resulting pressure
coefficient *c _{p}* is in well agreement with computations
using

*XFoil*and panel methods. (In order to increase the accuracy in the boundary region the computational grid also uses the boundary layer available with the

*gridgen*mesh generator).

The entire MATLAB m-script model file can be downloaded from the link below

Note that *fminbnd* will call both the FEA definition function and
solver in each minimization step which can become computationally
expensive for larger simulations. As done in the example it is
advisable to save and reuse as much data as possible, with the
*persistent* MATLAB argument, using old solutions as initial guesses,
or pre-computing and caching as much as possible.

A parametric study showing how the correction for the Kutta condition
effects the flow field for a NACA 4415 wing profile at 0 to 30 degrees
of angle of attack, can be seen in the video below.

Additional examples featuring optimization and parameter search can be found in the topology optimization example, and more on m-file script models can also be seen in the parametric study of the deflection of a bracket and bending of a wrench models and tutorials.