Increasing the efficiency of a heat exchanger

For our heat exchanger, we first need a CFD calculation. The boundary conditions are a total pressure of 100 Pa at the inlet, a static pressure of 0 Pa at the outlet and a heat flux of 10 W across the base plate. Thermal losses to the environment are neglected. The specification of a pressure gradient has the advantage over a mass flow boundary condition of preventing a potentially unfeasible constriction of the flow channel. The CFD analysis shows a clear non-uniform distribution of temperature and heat flux density between the four channels (see Fig.: 3 CFD results and sensitivities, No. 1 and No. 2).

The target variable in this case is obvious: the temperature averaged over the heated plate. For the Adjoint Solver, it initially does not matter whether it is a minimization or a maximization task, since this only results in sign reversed sensitivities. The direction of the sensitivities is only significant for post-processing and optimization. Initially, we work with first order discretization methods, since, to begin, the direction and location of the sensitivities are more important than their magnitude. Moreover, higher order methods provide the necessary additional accuracy only near an optimum. Optional stability methods help to improve the convergence behavior.

The plot of the sensitivity vectors shows that, in particular, the entrance region into the vertical channels has a large influence on the target variable (see Fig.:3 CFD results and sensitivities, No. 3). The vectors here indicate the direction in which the walls would have to be deformed to reduce the surface temperature of the heated slab. For a subsequent free-form optimization, this means that the largest changes are to be expected in this region. For parameter optimization, this gives us an indication of efficient geometry parameter placement. The sensitivity, with respect to the turbulence, shows that in the area of the channels, an increase of the turbulence near the wall would lead to a temperature reduction of the plate (see Fig.: 3 CFD results and sensitivities, No. 4).

The free-form optimization

The sensitivity-based free-form optimization is found under the menu item Gradient-Based Optimizer. Since the predictions of the sensitivities are linear, the path from the start design to the target design is divided into several design iterations. Here, a design iteration consists of 4 steps:

• Calculation of sensitivities
• Mesh Morphing
• Mesh optimization
• CFD calculation

For mesh morphing, Ansys Fluent offers three different morphing methods, which will be introduced in another article. The optimization is terminated when there is no more potential for improvement - we speak here of converged optimization.

Let's look at free-form optimization using our heat exchanger as an example. After three design iterations, the optimization has converged, reducing the averaged temperature of the heated plate by 5.5 K (about 7.5%). Comparing the temperature distribution before and after optimization, the four channels after optimization all have a similar fluid temperature, in contrast to the starting design (see Fig.: 4 Free-form optimization of the heat exchanger). In addition, the flow after optimization exhibits better mixing and thus increased convective heat transport.

Due to the free choice of the target variable, the Adjoint Solver can be applied to a wide range of problems. In this article, we have shown that not only can the free-form optimization be of interest, but also the sensitivities, which allow a deep insight into the design. Based on a single CFD analysis, areas can be identified that have a large impact with respect to a previously defined target variable. This deeper understanding can effectively support the design process and helps you to make targeted design changes.