NASA NTRS · 19830020939
Numerical Simulation for Droplet Combustion Using Lagrangian Hydrodynamics
Abstract
A 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.
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Fritts, M. J., Fyfe, D. E., Oran, E. S.. 1983-03-01. Numerical Simulation for Droplet Combustion Using Lagrangian Hydrodynamics. https://ntrs.nasa.gov/citations/19830020939
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