How Does Fuel/Air Ratio Affect Combustion Chamber Temperature in Turbojets?

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hi, I am studying aerospace engineering in oz, and I am doing an assignment on turbojet engines and I am looking for a chart on Combustion chamber temperature rise versus fuel air ratio with chamber inlet temperature as a parameter but I am having no luck lin finding one can anyone point me in the right direction.

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The only thing I can think of off the top of my head relates those parameters is the combustion efficiency. You would need to know that (among a couple of other terms) to calculate the temperature rise.