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On the Formation of Nitrogen Oxides During the Combustion of ...

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3 Experiments on Droplet Array <strong>Combustion</strong><br />

<strong>of</strong> typical hydrocarbon fuels <strong>of</strong> approximately 2000 K, substantial amounts <strong>of</strong><br />

CO and H 2 exist in equilibrium with CO 2 and H 2 O. However, by assuming that<br />

CO 2 and H 2 O are <strong>the</strong> only combustion products, <strong>the</strong> total heat <strong>of</strong> production<br />

is overpredicted. This effect was pointed out by <strong>the</strong> authors <strong>of</strong> <strong>the</strong> mechanism<br />

[459], and it is illustrated in Figure A.1 for C 10 H 22 . Here, <strong>the</strong> temperature<br />

difference in <strong>the</strong> flame and post-flame zone adds up to 170K, comparing<br />

<strong>the</strong> single-step mechanism used with <strong>the</strong> detailed kinetics <strong>of</strong> Zhao et al.<br />

[474]. Consequently, <strong>the</strong> results <strong>of</strong> this first numerical simulation may only<br />

be consulted for a first estimate <strong>of</strong> flame spread and are not suitable for any<br />

quantitative NO x studies, such as those involving NO x post-processing. In addition,<br />

<strong>the</strong>re are significant heat losses in <strong>the</strong> physical experiment due to radiation<br />

that are not accounted for within this basic CFD study. In this respect, a<br />

rough estimate <strong>of</strong> <strong>the</strong> real temperature rise due to combustion can be derived<br />

from <strong>the</strong> measurement readings plotted in Figures D.1 through D.3. Despite<br />

<strong>the</strong> <strong>the</strong>rmocouple positions some distance away from <strong>the</strong> flame zone and <strong>the</strong><br />

inertia <strong>of</strong> <strong>the</strong> system, <strong>the</strong> temperature increase observed remains low. Consequently,<br />

as expected, <strong>the</strong>re is a noticeable difference between physical experiment<br />

and <strong>the</strong> CFD study. Fur<strong>the</strong>rmore, Figure 3.22 clearly illustrates <strong>the</strong> fluid<br />

flow through <strong>the</strong> combustion chamber opening. In contrast to <strong>the</strong> present design,<br />

an idealized combustion chamber setup would foresee symmetry so that<br />

an even exhaust gas distribution could be maintained throughout <strong>the</strong> combustion<br />

process. However, this obvious design recommendation was beyond<br />

<strong>the</strong> scope <strong>of</strong> this design study.<br />

3.3.2 Fluid Dynamics <strong>During</strong> Exhaust Gas Sampling<br />

The second relevant gas exchange process <strong>of</strong> <strong>the</strong> combustion chamber is <strong>the</strong><br />

exhaust gas sampling itself, where evacuated sample cylinders collect <strong>the</strong><br />

combustion products. Position and orientation <strong>of</strong> <strong>the</strong> related sample probes<br />

inside <strong>the</strong> combustion chamber are important here, in particular in combination<br />

with <strong>the</strong> individual sampling approach for every single combustion run.<br />

Therefore, four symmetrically aligned probes were defined in <strong>the</strong> experiment<br />

specifications to allow a spatially uniform gas collection from <strong>the</strong> combustion<br />

chamber. The probe orifices were positioned as close as possible to <strong>the</strong> combustion<br />

zone, which facilitated a direct collection <strong>of</strong> <strong>the</strong> combustion products.<br />

Never<strong>the</strong>less, <strong>the</strong> ensuing gas exchange is even more complex than <strong>the</strong> one<br />

110

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