A mathematical
model for the operation of a thermal lance is developed
and validated, with the focus on its heat transfer and kinetics behavior.
It has been found that there is a “window” of combustion
rates in which the thermal lance can operate, which is mainly dictated
by the oxygen partial pressure. The particular value of the combustion
rate can be set by adjusting the flow rate of the oxygen supply, which
is practically done by manipulating the oxygen supply pressure. An
open issue is the lack of experimental kinetics data for thermal lance
combustion.