Comparison of the temperature in the combustion chamber of axial symmetry of help caused by changing air ratio per primary secondary. The basic values that can be used as a reference, which is 0.1538.
Comparing temperature axial symmetry of the combustion chamber allows the changing of the ratio of primary to secondary air. This value is based on quoted 0.1538.
Comparing the temperature in the axial symmetry of the combustion chamber to help caused by changing the value ratio per secondary, primary air The baseline reference is 0.1538.