Source terms for calculations of vaporizing and burning fuel sprays with non-unity Lewis numbers in gases with temperature-dependent thermal conductivities

Urzay, J., Pitsch, H. and Liñán Martínez, Amable ORCID: https://orcid.org/0000-0002-6161-8715 (2011). Source terms for calculations of vaporizing and burning fuel sprays with non-unity Lewis numbers in gases with temperature-dependent thermal conductivities. "Nasa-Stanford Annual Research Briefs" ; pp. 199-211.

Descripción

Título: Source terms for calculations of vaporizing and burning fuel sprays with non-unity Lewis numbers in gases with temperature-dependent thermal conductivities
Autor/es:
Tipo de Documento: Artículo
Título de Revista/Publicación: Nasa-Stanford Annual Research Briefs
Fecha: Diciembre 2011
Materias:
ODS:
Escuela: E.T.S.I. Aeronáuticos (UPM) [antigua denominación]
Departamento: Motopropulsión y Termofluidodinámica [hasta 2014]
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

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Resumen

Liquid-fueled burners are used in a number of propulsion devices ranging from internal combustion engines to gas turbines. The structure of spray flames is quite complex and involves a wide range of time and spatial scales in both premixed and non-premixed modes (Williams 1965; Luo et al. 2011). A number of spray-combustion regimes can be observed experimentally in canonical scenarios of practical relevance such as counterflow diffusion flames (Li 1997), as sketched in figure 1, and for which different microscalemodelling strategies are needed. In this study, source terms for the conservation equations are calculated for heating, vaporizing and burning sprays in the single-droplet combustion regime. The present analysis provides extended formulation for source terms, which include non-unity Lewis numbers and variable thermal conductivities.

Más información

ID de Registro: 34712
Identificador DC: https://oa.upm.es/34712/
Identificador OAI: oai:oa.upm.es:34712
URL Oficial: http://web.stanford.edu/~jurzay/Urzay2011CTR2.pdf
Depositado por: Biblioteca ETSI Aeronauticos
Depositado el: 16 Mar 2015 12:09
Ultima Modificación: 08 Feb 2023 08:24