Modelling turbulent combustion in a non-adiabatic Co/H2 flame using reaction progress variables

Jim B.W. Kok, Jurgen J.J. Louis

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

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Abstract

A model is presented for the turbulent combustion of CO/H2-air Mixtures at gas turbine conditions. The model takes account of heat losses. The conversion of CO to CO2 and of H2 to H2O, as well as the non-equilibrium intermediate species concentrations are determined by two reaction progress variables and two other scalar variables. The initially available fuel concentration is expressed by a fuel mixing variable. The heat loss effect on the enthalpy is described by a scaled enthalpy variable. The modelled turbulent source terms in the transport equations for the scalar variables are discussed. Three cases of a turbulent CO/H2 diffusion flame with heat loss and chemical super-equifibrium of intermediate species are presented.

Original languageEnglish
Title of host publicationASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
PublisherWeb Portal ASME (American Society of Mechanical Engineers)
VolumeVolume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
ISBN (Electronic)9780791878743
DOIs
Publication statusPublished - 1996
EventASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996 - Birmingham, United Kingdom
Duration: 10 Jun 199613 Jun 1996

Conference

ConferenceASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996
Country/TerritoryUnited Kingdom
CityBirmingham
Period10/06/9613/06/96

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