The turbofan is a combination of the turbine and a ducted fan. Reducing the propeller diameter and increasing the number of blades allows the fan to be aligned along the turbine axis. A shroud or the cover is used to improve the quality of flow through the fan. There are two airflow streams. One stream through the engine that is mixed with fuel, burnt and drives the turbine. The other over the engine.
GE T90 Turbofan
Turbofan Schematic
Turbofan ideal cycle (no fan)
Turbofan cutaway
An important parameter characterizing the turbofan is the bypass ratio:
Higher bypass ratio are associated with
lower specific fuel consumption
reduced noise
higher structural weight
higher engine drag
higher cost