The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor

This work addresses the prediction of the reacting flow field in a swirl stabilized gas turbine model combustor using large-eddy simulation. The modeling of the combustion chemistry is based on laminar premixed flamelets and the effect of turbulence-chemistry interaction is considered by a presumed...

Descripción completa

Detalles Bibliográficos
Autores principales: Gövert, Simon, Mira, Daniel, Kok, Jim B. W., Vázquez, Mariano, Houzeaux, Guillaume
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Springer Netherlands 2017
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6044246/
https://www.ncbi.nlm.nih.gov/pubmed/30069142
http://dx.doi.org/10.1007/s10494-017-9848-4

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6044246/
https://www.ncbi.nlm.nih.gov/pubmed/30069142
http://dx.doi.org/10.1007/s10494-017-9848-4

Ejemplares similares