Tutorials Manual
Tutorials Manual
Tutorials Manual
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Chapter 2: Combustion in Gas-phase Processes<br />
<strong>Tutorials</strong> <strong>Manual</strong><br />
processes in these flames is critical to interpreting flame experiments and to<br />
understanding the combustion process itself. Examples of the use of flame modeling<br />
to interpret experimental observations and to verify combustion chemistry and<br />
pollution formation can be found in Miller, et al. 9<br />
2.3.4.2 Project Setup<br />
The project file is called pre-mixed_burner__burner_stabilized.ckprj. The data files<br />
used for this sample are located in the<br />
samples41\pre-mixed_burner\burner_stabilized directory. This reactor model is<br />
simple and contains only one gas inlet and one premixed-burner reactor.<br />
On the Reactor Physical Properties tab of the C1_ Pre-Mixed Burner panel, the<br />
problem type is selected as Fix Gas Temperature because a measured temperature<br />
profile is used rather than computing the gas temperatures from the energy equation.<br />
For these laminar flames, the gas temperatures are often obtained from experiment<br />
rather than by solving an energy conservation equation. This is because there can be<br />
significant heat losses to the external environment, which are unknown or difficult to<br />
model. For cases where the heat losses are known or negligible, the user can solve a<br />
burner-stabilized flame problem in which the temperatures are determined from the<br />
energy conservation equation. Even if the energy equation is to be solved for the<br />
temperatures, the iteration converges more reliably if the species profiles are first<br />
computed using a fixed temperature profile. In any case, the user needs to input an<br />
estimate of the temperature profile. For this example, a temperature profile called<br />
pre-mixed_burner__burner_stabilized_TPRO.ckprf is input on the Reactor Physical<br />
Properties tab and only the species transport equations are solved using the<br />
temperature as a constraint. The system pressure (25 Torr) is also input on this panel,<br />
along with the choice of Mixture-averaged Transport and the use of the Correction<br />
Velocity Formalism.<br />
The Ending Axial Position (10 cm) for the simulation is input on the Initial Grid<br />
Properties tab of the C1_ Pre-Mixed Burner panel, along with a number of parameters<br />
concerning the gridding of the problem. A few of the grid parameters have been<br />
changed from the default values. The pre-mixed burner reactor model has adaptive<br />
gridding. The initial simulations are therefore done on a very coarse mesh that may<br />
have as few as five or six points. After obtaining a solution on the coarse mesh, new<br />
9. J. A. Miller, R. E. Mitchell, M. D. Smooke, and R. J. Kee, in Proceedings of the Nineteenth<br />
Symposium (International) on Combustion, The Combustion Institute, Pittsburgh,<br />
Pennsylvania, 1982, p. 181. J. A. Miller, M. D. Smooke, R. M. Green, and R. J.<br />
Kee, Combustion Science and Technology 34:149 (1983). J. A. Miller, M. C. Branch,<br />
W. J. McLean, D. W. Chandler, M. D. Smooke, and R. J. Kee, in Proceedings of the<br />
Twentieth Symposium (International) on Combustion, The Combustion Institute, Pittsburgh,<br />
Pennsylvania, 1985, p. 673.<br />
RD0411-C20-000-001 33 © 2007 Reaction Design