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I assume you're asking about the turbofans on passenger airliners, so that's what I'll describe. First, look up "high-bypass turbofans" for a picture.
The actual "engine" occupies only about the center third of the cowling you see hanging below the wing, the rest is air...
The engine provides the power to spin the fan (the blades you see from the front). The fan then moves a much larger amount of air through the duct (cowl) than a propeller would spinning in the open air. This is crucial for high altitude operation because the density of the air at altitude is so much less than at sea level that it's almost impossible to move a sufficient WEIGHT (not volume) of air backward to provide enough thrust for propulsion.

The cowl or duct improves the effiency of the fan by preventing the air from spilling off the tips of the fan blades. If you look at the wingtips of long-range aircraft like the 747-400, you'll see "fins" (winglets) sticking up from the wingtips. They do exactly the same thing aerodynamically as a duct except that it's for lift, not thrust.
For another interesting technology, look up "unducted fan". I think Lear has started using them now.


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This may be over-simplified, but jet engines are large because they have to produce a large amount of thrust due to the size of these passenger aircraft. During take-off, the turbo-fan engine can produce 50,000 lbs of thrust for each engine. That is tremendous compared to the older propellor technology.

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