Tutorials Manual
Tutorials Manual
Tutorials Manual
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Chemkin 4.1.1<br />
Chapter 2: Combustion in Gas-phase Processes<br />
third body efficiency for N is set to zero. And we add a new reaction<br />
N 2 + N = N + N + N to explicitly address the different temperature dependence of<br />
nitrogen atom as the third body. Figure 2-32 shows these two reactions in CHEMKIN<br />
format.<br />
Figure 2-32<br />
Nitrogen Atom Reaction in CHEMKIN Format<br />
N2+M=N+N+M 1.92E17 -0.5 224900.<br />
N2/2.5/ N/0/<br />
N2+N=N+N+N 4.1E22 -1.5 224900.<br />
2.5.1.2 Problem Setup<br />
Setting up a shock tube model requires information from the corresponding<br />
experiment. In addition to the conditions of the initial (unshocked) gas mixture, we will<br />
need to provide information on the diameter of the shock tube, the viscosity of the gas<br />
at 300 K, and the velocity of the incident shock. If we do not know the shock velocity<br />
from the experiment, we can estimate it by using the Equilibrium Reactor Model with<br />
the Chapmen-Jouguet detonation option. The shock tube diameter and the gas<br />
viscosity at 300 K are only required when the boundary-layer correction is used in the<br />
shock simulation.<br />
The project file, incident_shock__normal_air.ckprj, is stored in the samples41<br />
directory and the air dissociation mechanism by Camac and Feinberg is located in the<br />
associated working directory.<br />
2.5.1.3 Project Results<br />
The NO mole fraction behind the incident shock is shown in Figure 2-33 as a function<br />
of time. The NO mole fraction profile rapidly rises to a peak value then gradually falls<br />
back to its equilibrium level. Reasons for the greater-than-equilibrium peak NO<br />
concentration can be found in the paper by Camac and Feinberg and references<br />
therein. The predicted peak NO mole fraction is 0.04609 and is in good agreement<br />
with the measured and the computed data by Camac and Feinberg.<br />
© 2007 Reaction Design 56 RD0411-C20-000-001