Abstract
The use of pneumatic atomization of fuel in combustion chambers of jet engines permits a substantial increase in the completeness of combustion and a corresponding decrease in soot formation and exhaust of toxic substances. A mathematical model of the flame of a liquid-fuel pneumatic injector-nozzle, needed in the design of combustion chambers and other burner systems, is presently lacking. This has to do, first of all, with the problem of the mathematical description of a turbulent, two-phase reacting jet in a complex flowfield where the role of "two-phase" effects appears to be most important.
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