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Troels Dyhr Pedersen.indd - Solid Mechanics

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10 The reaction kinetics of DME<br />

- 33 - -<br />

10.1 Elementary reaction model<br />

All elementary reactions are modeled using the three parameter form of the Arrhenius<br />

expression:<br />

k(<br />

T ) = A ⋅T<br />

e<br />

with units<br />

T : K<br />

Cal<br />

E A :<br />

mol<br />

Cal<br />

RU<br />

:<br />

mol ⋅ K<br />

The unit of A depends on the reaction type.<br />

−E<br />

A <br />

b<br />

<br />

<br />

RU<br />

T <br />

<br />

<br />

The parameters needed to calculate the forward reaction rate coefficient are the frequency<br />

factor A, the temperature exponent b and the activation energy EA. These parameters are<br />

supplied for both forward and reverse reactions in the reaction mechanism used to model<br />

DME combustion.<br />

10.2 The detailed reaction scheme<br />

The reaction kinetics of DME is described in details by a reaction scheme named DME<br />

2000 from Lawrence Livermore National Laboratory. The reaction scheme is based on<br />

studies on premixed DME/air flames at atmospheric pressure. Extensive documentation is<br />

available for this scheme [21]. Units are in mol, Calories and Kelvin.<br />

Low pressure and Troe fall-off corrections are given for some reactions. The details of<br />

these corrections are beyond the scope of this report, but the corrections are included in<br />

the simplified scheme for completeness.<br />

10.3 Reducing the mechanism for lean combustion<br />

The full scheme was developed to model both lean and rich flames. Rich flames involve<br />

much more complicated reaction paths than lean flames. Reactions leading to the<br />

formation of higher hydrocarbons are included, such as ethylene. Since ethylene is<br />

believed to be an important precursor to soot, the mechanism can potentially be used to<br />

predict soot formation in rich flames. The formation of higher hydrocarbons is however<br />

very low at lean and premixed conditions, since the possibility of local rich combustion<br />

zones is very limited. Hence there is no need to include these species in the description of<br />

lean combustion.

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