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 />
and Oxidizer specified. This is defined on the Complete-Combustion Products subtab.<br />
In this case, the product species are H 2 O and N 2 , where N 2 is included (because<br />
it is part of the fuel and oxidizer mixtures). Note that all of the elements contained in<br />
the fuel and oxidizer species must also appear in the product species.<br />
For this example, there are no inputs on the Basic tab of the Solver panel. We use the<br />
default settings, in which the application first solves a fixed-temperature problem and<br />
then uses the results of this solution as the initial guess to solve the full problem<br />
including the energy equation. On the Advanced tab of the Solver panel, the minimum<br />
bonds of species fractions have been specified as smaller than the default, to aid in<br />
convergence to a physical solution.<br />
On the Continuations panel, 8 additional simulations are specified where the<br />
equivalence ratio is gradually changed. There are no inputs on the Output Control<br />
panels for this problem, since default output options will be used.<br />
2.3.1.3 Project Results<br />
Figure 2-2 shows the steady-state temperatures for the combusting<br />
hydrogen/air/nitrogen mixture. In this case, the temperature peaks at a fuel/air<br />
equivalence ratio or about 1.25. As shown by the molar conversions in Figure 2-3,<br />
neither the fuel nor the oxidizer is completely consumed in this combustor, as a result<br />
of the PSR residence time.<br />
To get the plot in Figure 2-3, be sure to select the “molar_conversion” in the Select Results<br />
panel when the Post-Processor is first launched.<br />
Figure 2-2<br />
Steady-state Gas-phase Combustion—Hydrogen/Air Temperatures<br />
RD0411-C20-000-001 23 © 2007 Reaction Design