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Optimization and Computational Fluid Dynamics - Department of ...

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48 Gábor Janiga<br />

y [mm]<br />

18<br />

16<br />

14<br />

12<br />

10<br />

8<br />

6<br />

4<br />

2<br />

0<br />

-2<br />

CO<br />

0.085<br />

0.08<br />

0.075<br />

0.07<br />

0.065<br />

0.06<br />

0.055<br />

0.05<br />

0.045<br />

0.04<br />

0.035<br />

0.03<br />

0.025<br />

0.02<br />

0.015<br />

0.01<br />

0.005<br />

0<br />

HCO<br />

8.4E-05<br />

7.9E-05<br />

7.4E-05<br />

6.9E-05<br />

6.4E-05<br />

5.9E-05<br />

5.4E-05<br />

4.9E-05<br />

4.4E-05<br />

3.9E-05<br />

3.4E-05<br />

2.9E-05<br />

2.4E-05<br />

1.9E-05<br />

1.4E-05<br />

9E-06<br />

4E-06<br />

-10 -5 0 5 10<br />

x [mm]<br />

Fig. 2.18 Mass fraction field <strong>of</strong> CO (left) <strong>and</strong> HCO (right) in the worst feasible case for<br />

the EA optimization<br />

erence. In this way, the optimization problem involves several concurrent<br />

objectives that must be fulfilled simultaneously. Generic <strong>and</strong> robust search<br />

methods, such as EA, can be used for such problems as demonstrated here.<br />

The present optimization problem consists <strong>of</strong> finding the best group <strong>of</strong> values<br />

for the model constants <strong>of</strong> the k–ω turbulence model [79] leading to the most<br />

accurate prediction <strong>of</strong> the velocity distribution, in agreement with the DNS<br />

data. The k–ω model is widely used in CFD, demonstrating the importance<br />

<strong>of</strong> this issue. In a first investigation, the shear-stress pr<strong>of</strong>iles have been also<br />

examined, but the differences were quite small compared with DNS. It was<br />

observed that the constants producing a good velocity pr<strong>of</strong>ile automatically<br />

lead to an accurate shear-stress distribution as well, which is not unexpected,<br />

since the shear-stress directly depends on the velocity gradients. Therefore,<br />

the shear-stress pr<strong>of</strong>iles are dropped from the objectives <strong>and</strong> the number <strong>of</strong><br />

reference cases is increased, involving different Reynolds numbers.<br />

2.5.1 Governing Equations<br />

The Reynolds-averaged governing equations that describe turbulent flow motion<br />

are summarized here following Wilcox [79]. An incompressible flow with<br />

constant thermodynamic properties is now assumed, unlike Case B.

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