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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

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