Image: Jet engine numbered

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Description: Diagram of a typical gas turbine jet engine. Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor fan blades. Intake Low pressure compression High pressure compression Combustion Exhaust Hot section Turbines Low and High pressure Combustion chambers Cold section Air inlet
Title: Jet engine numbered
Credit: Own work, vector version of en:Image:FAA-8083-3A Fig 14-1.PNG which comes from an FAA handbook
Author: Jeff Dahl
Usage Terms: Creative Commons Attribution-Share Alike 4.0
License: CC BY-SA 4.0
License Link: https://creativecommons.org/licenses/by-sa/4.0
Attribution Required?: Yes

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