Jet Propulsion/Thermodynamic Cycles/Turbofan cycle
Jump to navigation Jump to search
The fan allows a reduction in the average exhaust velocity compensated by a larger mass flow for a given thrust.
Modern military aircraft use afterburning of combined bypass and core flows for high augmentation ratios.
| This page or section is an undeveloped draft or outline.
You can help to develop the work, or you can ask for assistance in the project room.