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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

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