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

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4.6 Model Validation<br />

utilized model accounts for gradients in <strong>the</strong> r -direction, transient effects <strong>of</strong><br />

droplet heating can be resolved correctly on an appropriate scale. The liquid<br />

phase model resembles <strong>the</strong> so-called “conduction limit” or “diffusion limit”<br />

model due to Law and Sirignano [236], which is recommended if <strong>the</strong> droplet<br />

Reynolds number is negligible compared to unity [9, 236, 381, 402, 403]. Comparing<br />

<strong>the</strong> <strong>the</strong>rmal diffusivities α <strong>of</strong> <strong>the</strong> liquid and gas phase yields α l ≪ α g .<br />

Thus, <strong>the</strong> transport processes in <strong>the</strong> gas phase happen much faster than in <strong>the</strong><br />

liquid phase, and <strong>the</strong> gas phase may be treated as quasi-steady.<br />

Figures 4.5 and 4.6 clarify <strong>the</strong> temperature sensitivity <strong>of</strong> <strong>the</strong> utilized single<br />

droplet model. In particular, Figure 4.5 shows <strong>the</strong> temperature distribution<br />

inside a water droplet during <strong>the</strong> initial, transient heating with T l,0 = 283.15 K<br />

and T ∞ = 473.15 K. At t = 1×10 −3 s, <strong>the</strong> droplet surface temperature T S is highest<br />

due to <strong>the</strong> initialization <strong>of</strong> <strong>the</strong> computational domain. However, it decreases<br />

immediately, before it starts to increase continuously, while accounting<br />

for <strong>the</strong> heat flux from <strong>the</strong> gas phase into <strong>the</strong> droplet. In Figure 4.6, water<br />

droplets are vaporized in an ambient gas environment at T ∞ = 473 K with different<br />

initial temperatures <strong>of</strong> <strong>the</strong> liquid phase (283, 303, 323, 343, and 363 K).<br />

The respective wet-bulb temperatures are reached after 3 to 10% <strong>of</strong> <strong>the</strong> droplet<br />

lifetime, depending on <strong>the</strong> temperature difference between T l,0 and T ∞ . All<br />

wet-bulb temperatures match with a relative humidity on <strong>the</strong> droplet surface<br />

in <strong>the</strong> range <strong>of</strong> ϕ= 10%. Hence, <strong>the</strong> heat transfer inside <strong>the</strong> droplet as well as<br />

heat and mass transfer over <strong>the</strong> gas-liquid interface show a correct and consistent<br />

behavior. As far as <strong>the</strong> experiments on droplet array combustion (Chap. 3)<br />

are concerned, <strong>the</strong> heating phase <strong>of</strong> <strong>the</strong> droplets is significant and cannot be<br />

neglected. It must be included in <strong>the</strong> calculation <strong>of</strong> <strong>the</strong> pre-vaporization rate<br />

Ψ (see also Tabs. D.1 through D.3).<br />

4.6.1 Validation <strong>of</strong> Vaporization Mechanism Without <strong>Combustion</strong><br />

Since <strong>the</strong> calculated vaporization rate k is a fur<strong>the</strong>r indicator <strong>of</strong> <strong>the</strong> accuracy <strong>of</strong><br />

<strong>the</strong> simulation results, it is evaluated for water and n-decane droplets against<br />

<strong>the</strong> classical D² law as well as experimental measurements. Ansatz, assumptions,<br />

and resulting equations are discussed here. In order to facilitate <strong>the</strong><br />

comparison <strong>of</strong> <strong>the</strong> simulation results with <strong>the</strong> simplified validation model, <strong>the</strong><br />

vaporization process is studied as an example for droplets in an atmosphere<br />

<strong>of</strong> air.<br />

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