Combustion Temperature

The temperature after combustion primarily based on the inlet air temperature, and the quantity of thermal energy released per unit mass of mixture, that is mainly a function of the FAR.

The combustion temperature fall off around half as quickly with a rise in FAR above the stoichiometric value as does the heating value of fuel, since of the high quantity of fuel present per unit mass of air. Gas turbines and combustion engines are exemplified by high combustion temperatures, resultant from the air compression former to combustion.