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Optimization and Computational Fluid Dynamics - Department of ...

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258 Marco Manzan, Enrico Nobile, Stefano Pieri <strong>and</strong> Francesco Pinto<br />

10<br />

8<br />

f/f<br />

0 6<br />

4<br />

2<br />

Linear−piecewise wall pr<strong>of</strong>ile<br />

NURBS wall pr<strong>of</strong>ile<br />

1 1.1 1.2 1.3 1.4 1.5 1.6 1.7<br />

Nu/Nu<br />

0<br />

Fig. 8.20 Pareto front comparison between linear piecewise <strong>and</strong> NURBS-based channels<br />

<strong>and</strong> longitudinal steady vortices on the heat transfer rate is again clear. For<br />

illustrative purposes, the secondary flow pattern for two channels obtained<br />

with a 20 ◦ <strong>and</strong> 40 ◦ extrusion respectively, are depicted in Fig. 8.22.<br />

Finally, a MOGA optimization has been started on extruded linear piecewise<br />

channels for a short number <strong>of</strong> generations. The Pareto front <strong>of</strong> this<br />

optimization is compared in Fig. 8.23 with the 2D linear piecewise <strong>and</strong> 2D<br />

NURBS fronts. Though the 3D linear piecewise front is rather sparse because<br />

<strong>of</strong> a small number <strong>of</strong> individuals processed, the heat transfer augmentation<br />

due to secondary motions is clearly visible.<br />

8.8.5 CC Module<br />

Again with MOGA-II, an original design was used for the DOE when optimization<br />

was first attempted. The design had sinusoidal wall pr<strong>of</strong>ile (design<br />

0), characterized by a corrugation angle θ =60 ◦ , <strong>and</strong> 35 designs have<br />

been chosen with Sobol method. The value <strong>of</strong> the angle θ has been chosen,<br />

following Stasiek et al. [52], as a good compromise in terms <strong>of</strong> heat transfer<br />

rate <strong>and</strong> friction factor. The six design variables were, with reference to<br />

Fig. 8.6, P1, P2, P3, P4, W <strong>and</strong> θ. The three objectives to be minimized<br />

were the pressure gradient β, the temperature difference between the two<br />

fluids ∆T <strong>and</strong> the heat transfer surface area. The first objective has been<br />

selected to reduce the pressure drop across the regenerator. The second one<br />

drives the heat transfer performance <strong>of</strong> the regenerator. For instance, based<br />

on inspection <strong>of</strong> Eq. (8.35), a lower ∆T leads to a higher mean Nusselt number.<br />

The last objective has been selected to reduce the overall cost <strong>of</strong> the

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