High Bypass Turbofan Jet Engine Model 2

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A High Bypass Turbofan Jet Engine's key components are the nacelle, fan, 2-stage low pressure compressor, 3-stage high pressure compressor, combustion chamber, 3-stage high pressure turbine, 2-stage low pressure turbine, core nozzle, and fan nozzle. The engine's working process starts with the inlet capturing incoming air. Some of this air passes through the fan, then into the core compressor, and finally the burner for combustion. The hot exhaust exits via the core and fan turbines and nozzles, similar to a turbojet. The remaining incoming air bypasses the engine, similar to a propeller's airflow. This fan-driven air has slightly increased velocity, contributing to the engine's thrust, with the ratio of bypassed air to core air known as the bypass ratio. This topic was presented in my final seminar. Check out my YouTube channel for more details: https://www.youtube.com/channel/UCzFRwBLs5z_HmyOp_jiPKNg