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Title: A study of droplet burning in the nearly adiabatic limit
Author: Gomez, Juan C.
View Online: njit-etd2000-019
(vii, 108 pages ~ 5.1 MB pdf)
Department: Department of Mathematical Sciences
Degree: Doctor of Philosophy
Program: Mathematical Sciences
Document Type: Dissertation
Advisory Committee: Booty, Michael R. (Committee chair)
Kriegsmann, Gregory A. (Committee member)
Bechtold, John Kenneth (Committee member)
Luke, Jonathan H.C. (Committee member)
Rosato, Anthony D. (Committee member)
Date: 2000-05
Keywords: Liquid fuel
Oxidizing gaseous environment
Adiabatic burning
Availability: Unrestricted

We consider a small drop of liquid fuel that burns in an oxidizing gaseous environment and translates slowly (relative to flow 'at infinity') under the action of gravity. Practical applications include the burning of liquid fuels as sprays in domestic and industrial oil-fired burners, diesel engines, and liquid-propellant rocket motors. More relevant to the simple physical set-up of the present study are wellcharacterized laboratory experiments on the burning of a single, isolated fuel drop.

The drop burns in a nearly spherical, diffusion flame, flame sheet regime. We consider a specific example, or limit, referred to as 'nearly adiabatic burning', in which the temperature of the gas mixture at the flame sheet is close to the ambient temperature at infinity. Temperature gradients everywhere outside the flame sheet are therefore small. The problem is solved by perturbation methods, primarily, with a distinguished limit between the inverse nondimensional activation energy ε and the translational Reynolds number Re. We include time dependence far from the drop as a quasisteady effect, and this influences the near field region of the drop via matching between near field and far field.

Evaluation of quantities such as the 'drag' force exerted by the fluid on the drop, the flame sheet shape, and the speed of translation necessitates numerical solution of a higher order problem in the perturbation scheme. Results predicted for the behavior of a heptane fuel drop will be presented.

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