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Numerical Simulation for Droplet Combustion Using Lagrangian HydrodynamicsA predictive model of spray combustion must incorporate models for the wide variety of physical environments in a practical combustor. In regions where droplets are closely spaced, combustion resembles a diffusion flame; where they are well separated, an envelope or wake flame results. The relative velocity field between the fuel droplets and oxidizer in influences boundary layer development about the droplet, recirculating flow patterns, and droplet shape and stability. A model must encompass these interacting temporal and spatial effects as well as complicated combustor boundaries. The objective of the current work is to develop the triangular gridding method for describing the individual and collective properties of vaporizing and burning fuel droplets.
Document ID
19830020939
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fritts, M. J.
(Naval Research Lab. Washington, DC, United States)
Fyfe, D. E.
(Naval Research Lab. Washington, DC, United States)
Oran, E. S.
(Naval Research Lab. Washington, DC, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Aircraft Propulsion And Power
Accession Number
83N29210
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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