Temperature of the back of a turbine jet engine (or something like that)

AI Thread Summary
The temperature at the back of a turbine jet engine varies significantly based on the engine type and operating conditions, particularly between high-bypass and low-bypass designs. For modern fighter jets, the exhaust temperatures can be quite high, but specific figures depend on the engine model and its operational state. A useful resource for understanding these variations is the Wikipedia page on jet engines, which provides detailed information on combustion temperatures and engine types. Users seeking precise data for calculations should consider the specific engine type they are examining. This information is essential for accurate experimentation and design calculations.
strawmilk
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can anybody please tell me the temperature (degrees Celsius please.) there is at the back of a normal turbine jet engine (or something like that:-p )?? i couldn't find it on wikipedia or something like that:frown: so i ask it here:approve:
 
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There is an extremely wide range - could you be more specific as to what type and under what operating conditions?
 
hmm
i think the types used in modern fighter planes, in the air or something
i need the temperatures for calculations for my idea
 
There is a pretty good introductory treatment of the different types of jet engines at wikipedia.org:

http://en.wikipedia.org/wiki/Jet_engine

As Russ says, and as the article discusses, different jet engine types have different exhaust temperatures. High-bypass designs obviously cool off the exhaust more than low-bypass types. The temperature of the combustion is given about 2/3 of the way down the long page.
 
thank you very much
now i can go on calculating and experimenting ;)
 
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