Discussion Overview
The discussion revolves around the temperature at the back of turbine jet engines, specifically in the context of modern fighter planes. Participants seek to clarify the temperature range under various operating conditions for use in calculations and experiments.
Discussion Character
- Exploratory, Technical explanation, Homework-related
Main Points Raised
- One participant asks for the temperature at the back of a normal turbine jet engine, specifying a preference for degrees Celsius.
- Another participant notes the wide range of temperatures and requests more specific details regarding the type of engine and operating conditions.
- A participant mentions interest in temperatures for modern fighter planes and indicates the need for this information for calculations related to their idea.
- Reference is made to an introductory treatment of jet engines on Wikipedia, highlighting that different types of jet engines have varying exhaust temperatures, with high-bypass designs cooling the exhaust more than low-bypass types.
- A participant expresses gratitude after receiving information, indicating they can proceed with their calculations and experiments.
Areas of Agreement / Disagreement
Participants do not reach a consensus on a specific temperature, as the discussion highlights the variability based on engine type and operating conditions.
Contextual Notes
The discussion lacks specific assumptions about the types of engines or conditions being referenced, and the temperature ranges remain unresolved.
)?? i couldn't find it on wikipedia or something like that
so i ask it here