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In aero engine combustors, dilution air jets are used to additionally tailor the temperature field, the emissions, and the turbine inlet profile. These jets are entering the combustion chamber at different axial and circumferential locations through
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::44e8dd5b5ef0e1ff4d84deff3ba21eee
https://doi.org/10.1115/1.0002863v
https://doi.org/10.1115/1.0002863v
Publikováno v:
Volume 4A: Combustion, Fuels, and Emissions.
This paper considers a variation on Conditional Moment Closure (CMC) modelling for turbulence-chemistry interaction called the Uniform Conditional State (UCS) model and its application to the prediction of swirl-stabilized flames. UCS is essentially
Publikováno v:
Volume 5C: Heat Transfer.
The numerical description of combustion provides a good understanding of the thermal boundary conditions of a combustor already in the early design phase. With an accurate simulation, the thermal load on the combustor wall as well as the turbine inle