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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 />

Figure 2-33<br />

Shock Tube Experiment—NO Mole Fraction<br />

2.6 Combustion in Complex Flows<br />

2.6.1 Gas Turbine Network<br />

2.6.1.1 Problem description<br />

2.6.1.2 Problem setup<br />

This tutorial utilizes a PSR-PFR network to predict NO x emission from a gas turbine<br />

combustor.<br />

A PSR network or a hybrid PSR-PFR network is commonly used to simulate mixing<br />

and flow characteristics of a gas turbine combustor. 16,17 This reactor network<br />

approach can greatly reduce the computational burden yet provide reasonable<br />

solutions for a complicated combustion process. However, constructing such a<br />

reactor network is rather empirical. Slight changes in combustor operating conditions<br />

often lead to a new reactor network configuration with a different number of reactors<br />

and connectivity. To speed up the time-consuming trial-and-error process, the<br />

CHEMKIN Interface provides a Diagram View that facilitates building and modification<br />

of a reactor network. A gas turbine reactor network is shown in Figure 2-35. Typically,<br />

a gas turbine reactor network consists of a flame/ignition zone, a recirculation zone,<br />

and a post-flame zone. However, depending on how the fuel and oxidizer are<br />

delivered and the complexity of the flow field, additional reactors and inlets may be<br />

needed to properly represent the combustor. The reactor network shown in<br />

16. A. Bhargava et al., J of Engineering for Gas Turbines and Power 122:405-411 (2000).<br />

17. T. Rutar and P.C. Malte, J of Engineering for Gas Turbines and Power 124:776-783<br />

(2002).<br />

RD0411-C20-000-001 57 © 2007 Reaction Design

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