Laminar mixing in diluted and undiluted fuel jets upstream from lifted flames

Revuelta Bayod, Antonio; Sánchez Pérez, Antonio Luis y Liñán Martínez, Amable (2002). Laminar mixing in diluted and undiluted fuel jets upstream from lifted flames. "Combustion and Flame", v. 128 (n. 3); pp. 199-210. ISSN 0010-2180.

Descripción

Título: Laminar mixing in diluted and undiluted fuel jets upstream from lifted flames
Autor/es:
  • Revuelta Bayod, Antonio
  • Sánchez Pérez, Antonio Luis
  • Liñán Martínez, Amable
Tipo de Documento: Artículo
Título de Revista/Publicación: Combustion and Flame
Fecha: Febrero 2002
Volumen: 128
Materias:
Palabras Clave Informales: Air; Approximation theory; Asymptotic stability; Boundary layers; Hydrocarbons; Jet aircraft; Laminar flow; Liquid fuels; Method of moments; Reynolds number; Stoichiometry; Laminar mixing; Lifted flames; Combustion; fuel; hydrocarbon; flame; gas-gas mixing; jet; laminar jet; accuracy; article; calculation; dilution; fire; flow rate; priority journal
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

The boundary-layer approximation is used to describe the frozen mixing process taking place when a fuel jet of radius a discharges into stagnant air. The results are applicable to the calculation of lifted flames stabilized in round laminar jets with relatively large Reynolds numbers, Re, for which the proposed formulation provides a detailed description for the velocity and composition fields encountered by the propagating triple flame formed at the base of the lifted flame. The problem is integrated for relevant values of the flow parameters, including values of the stoichiometric air-to-fuel mass ratio S of order unity, when the lifted flame is located in the region of jet development, corresponding to distances from the injector of order Re a. Further attention is given to the relevant case S ≫ 1, corresponding to typical conditions of undilute hydrocarbon-air flames, for which the resulting lifted flames are stabilized at relatively large distances from the injector, of order S Re a. It is seen that Schlichting asymptotic solution, which corresponds to a point source of momentum, is then applicable to describe the mixing process upstream from the lifted flame. Improved accuracy is sought by introducing expansions for the velocity components and for the reactant mass fractions in powers of S-1. The resulting development shows in particular that the first-order correction to the leading-order solution is equivalent to the introduction of a virtual origin for the axial coordinate. It is shown that the magnitude of the required translation, which is equal for the velocity and composition fields, must be determined from continuity considerations. As an illustrative example, the resulting description is used to calculate flame fronts with S ≫ 1 in the thermal-diffusive approximation.

Más información

ID de Registro: 852
Identificador DC: http://oa.upm.es/852/
Identificador OAI: oai:oa.upm.es:852
URL Oficial: http://www.sciencedirect.com/science/journal/00102180
Depositado por: Archivo Digital UPM
Depositado el: 09 Feb 2008
Ultima Modificación: 20 Abr 2016 06:33
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