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TECHNICAL PAPERS: Gas Turbines: Combustion and Fuels

Numerical Simulation of Swirl-Stabilized Premixed Flames With a Turbulent Combustion Model Based on a Systematically Reduced Six-Step Reaction Mechanism

[+] Author and Article Information
D. E. Bohn

J. Lepers

Institute of Steam and Gas Turbines, Aachen University of Technology, Templergraben 55, Aachen 52056, Germany

J. Eng. Gas Turbines Power 123(4), 832-838 (Oct 01, 2000) (7 pages) doi:10.1115/1.1377597 History: Received October 01, 1999; Revised October 01, 2000
Copyright © 2001 by ASME
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References

Figures

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Numerical discretization
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Numerical results for combustion at 1 atm and TIN=300 K
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Species distributions at axial positions x/Do=0.5 and x/Do=1.0 (1 atm, TIN=300 K)
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Boundary conditions for computations under typical gas turbine combustor inlet conditions
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Comparison of computations for atmospheric and elevated pressure
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Concentrations of nitrogen oxides at axial position x/Do=1.0

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