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

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A.2 Concepts <strong>of</strong> Kinetics Reduction<br />

power, <strong>the</strong> net reaction rates <strong>of</strong> <strong>the</strong> latter can be set to zero, leading to algebraic<br />

relations. The steady-state approximation searches for species whose<br />

production and consumption cancel out immediately. By doing so, many intermediate<br />

species can be eliminated from a detailed mechanism if <strong>the</strong>ir net<br />

production rates tend towards zero. In practice, species are regarded as quasisteady<br />

if <strong>the</strong>ir net production rate is small compared to <strong>the</strong>ir respective production<br />

and consumption rates [11, 43, 336]. This process <strong>of</strong> analyzing <strong>the</strong><br />

timescales was successfully automated, resulting in <strong>the</strong> so-called computer<br />

assisted reduction method (CARM). It evaluates reaction rates and automatically<br />

eliminates species at quasi-steady state on <strong>the</strong> basis <strong>of</strong> results obtained<br />

from perfectly stirred reactor models, employing more or less detailed mechanisms<br />

[67, 90, 299].<br />

The computational singular perturbation (CSP) method investigates <strong>the</strong> dynamics<br />

<strong>of</strong> <strong>the</strong> source term vector and tries to find <strong>the</strong> directions in which it<br />

will rapidly reach steady-state. Eigenvalues and eigenvectors <strong>of</strong> <strong>the</strong> Jacobian<br />

matrix <strong>of</strong> <strong>the</strong> source term represent chemical timescales and reaction groups,<br />

respectively [11, 43, 256].<br />

The intrinsic low-dimensional manifold (ILDM) method was presented by<br />

Maas and Pope [262] in 1992. Similar to <strong>the</strong> CSP method, <strong>the</strong> ILDM method<br />

tries to find directions in state space in which <strong>the</strong> source term rapidly reaches<br />

steady-state. The method is based on <strong>the</strong> assumption that a combustion system<br />

follows certain trajectories in state space during <strong>the</strong> combustion process.<br />

However, <strong>the</strong>se trajectories are not associated with any particular species or<br />

reaction. Since <strong>the</strong> steady-state assumption is applied locally, different reaction<br />

paths can be captured. The common part <strong>of</strong> all trajectories can be described<br />

as a parameterized curve <strong>of</strong> only a single progress variable. Assuming<br />

all but two processes to be in steady-state results in a surface parameterized<br />

by two variables and so on. This process generally leads to intrinsic lowdimensional<br />

manifolds, in which <strong>the</strong> number <strong>of</strong> dimensions represents <strong>the</strong><br />

number <strong>of</strong> slow processes. However, <strong>the</strong> higher <strong>the</strong> number <strong>of</strong> dimensions,<br />

<strong>the</strong> more rapidly <strong>the</strong> trajectories through state space will approach <strong>the</strong> manifold.<br />

As time approaches infinity and independently <strong>of</strong> <strong>the</strong> initial conditions,<br />

all solution trajectories <strong>of</strong> stable systems will approach <strong>the</strong> same equilibrium<br />

point. Thus, movement along <strong>the</strong> ILDM corresponds to <strong>the</strong> evolution <strong>of</strong> <strong>the</strong><br />

predefined slow processes, and <strong>the</strong> equilibrium point effectively would be a<br />

zero-dimensional manifold [191, 262, 399, 400].<br />

203

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