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

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4 Numerical Modeling and Simulation<br />

Equations (4.36) through (4.38) yield a transcendental equation for <strong>the</strong> determination<br />

<strong>of</strong> <strong>the</strong> <strong>of</strong>fset radius ∆r . Finally, <strong>the</strong> total amount <strong>of</strong> heat Q introduced<br />

in or extracted from <strong>the</strong> system needs to be defined by <strong>the</strong> user. It delivers<br />

<strong>the</strong> maximum volumetric heat source ˙q v,max .<br />

Two different parameter sets realize <strong>the</strong> heat introduction and extraction process<br />

within <strong>the</strong> numerical model, indicated by “in” and “ex”, respectively.<br />

Finding appropriate values for <strong>the</strong> ignition parameters is crucial regarding<br />

NO x emissions. The parameters must be set to ensure a safe ignition, but NO x<br />

emissions are expected to depend on <strong>the</strong> amount <strong>of</strong> introduced heat Q in , position<br />

<strong>of</strong> <strong>the</strong> heat source r m,in , and ignition volume V in [297, 298].<br />

The amount <strong>of</strong> heat introduced by <strong>the</strong> heat source is Q in = 3×10 −3 J, which<br />

is about 20% <strong>of</strong> <strong>the</strong> lower heating value times <strong>the</strong> mass <strong>of</strong> <strong>the</strong> investigated<br />

fuel droplet 3 (see Chap. 5.2). The same amount <strong>of</strong> heat is nominally extracted<br />

from <strong>the</strong> computational domain with Q ex = −3.0×10 −3 J during droplet burning<br />

(cf. Fig. 4.2). To avoid negative effects, <strong>the</strong> absolute amount <strong>of</strong> heat |Q|<br />

is optimized to be as low as possible but still high enough to ensure ignition.<br />

The associated times are t in,min = 0.0ms and t in,max = 0.5ms as well as<br />

t ex,min = 1.0 ms and t ex,max = 1.5 ms, with a calculative time shift between heat<br />

introduction and extraction <strong>of</strong> ∆t = 1.0 ms. These time scales are chosen according<br />

to correlations given in Mikami et al. [282, 283] and Oyagi et al. [327]<br />

for <strong>the</strong> flame spread rate along droplet arrays. The experiments <strong>of</strong> Mikami<br />

et al. [283] show that <strong>the</strong> flame spread rate is<br />

v f D 0 = 50mm 2 s −1 (4.39)<br />

for an inter-droplet distance <strong>of</strong> S ≈ 10D 0 and a preheating temperature <strong>of</strong><br />

T = 600K. v f denotes <strong>the</strong> mean velocity <strong>of</strong> <strong>the</strong> flame front and can be expressed<br />

as<br />

v f = S<br />

τ ign<br />

, (4.40)<br />

where τ ign is <strong>the</strong> time between <strong>the</strong> ignition <strong>of</strong> two neighboring droplets. Solving<br />

for time yields<br />

τ ign = S D 1 s<br />

0·<br />

50 mm ≈ D 0· 2 1 s<br />

2 5 mm = 2 2.0×10−3 s. (4.41)<br />

3 The droplet itself has an initial diameter <strong>of</strong> D 0 = 100µm before <strong>the</strong> start <strong>of</strong> pre-vaporization.<br />

132

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