The paper reviews progress in the development of methods for calculating th
e properties of gas turbine combustion chambers, with particular attention
being devoted to combustion and turbulence-combustion interactions. For con
ventional combustion chambers with non-premixed combustion it is argued tha
t a conserved scalar approach, where burning is presumed to be 'fast', is c
apable of providing an accurate representation of heat-releasing processes.
The approach can also be extended to include NO2 formation, at least under
conditions where it is formed under high-temperature conditions. However,
if carbon monoxide and unburnt hydrocarbon emissions or partially premixed
combustion is to be considered, then a more complete description of combust
ion is needed and the probability density function (PDF) transport equation
method here represents a promising approach. It is demonstrated that the m
ethod, when combined with a simple chemical reaction mechanism, is capable
without modification of reproducing the major properties of non-premixed, p
artially premixed and premixed turbulent flames.