turbofan v slovarju Oxford-Hachette French Dictionary

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This engine is a dual rotor, axial flow, high bypass ratio turbofan.
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A turbojet engine equipped with an afterburner is called an afterburning turbojet, whereas a turbofan engine similarly equipped is sometimes called an augmented turbofan.
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A very low specific thrust (i.e. very high bypass ratio) turbofan is proposed for the aircraft.
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For turbojets the gain is limited to 50%, while it depends on the bypass ratio in a turbofan and can be as much as 70%.
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In a bid for increased efficiency with speed, a development of the "turbofan" and "turboprop" known as a propfan engine was created that had an unducted fan.
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This feature, related to the high bypass ratio turbofan, reduces the noise from the engines and improves fuel efficiency.
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Owing to the low specific thrust, the bypass ratio for the engine is higher than normal for a military turbofan.
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Taking the principle a step further, the high-bypass turbofan is even more efficient, having typically three spools each spinning at a different speed.
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It was a conventional design for its class, a low-wing monoplane with turbofan engines mounted in rear fuselage nacelles.
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Because of the implied low mean jet velocity, a high bypass ratio/low specific thrust turbofan has a high thrust lapse rate (with rising flight speed).
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