Topic: Turbofan Different from Turbojet
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Answers to Common Questions
What's the difference between a turbofan and a turbojet?
Turbo Fans. Use a fan at the front of the engine to produce most of its thrust. Where as a turbo jet uses all of the exhaust gases to produce all of its thrust. The main advantage of turbo fans is that they are a lot quieter Read More »
Source: http://answers.yahoo.com/question/index?qid=20090907221350AAbFxq6
What is the difference between a turbojet engine and a turbofan e...
A turbojet engine has a turbine that drives a compressor; tur... Read More »
Source: http://www.chacha.com/question/what-is-the-difference-between-a-t...
What is the difference between a turboprop, turbofan and turbojet...
A turbojet is your basic jet engine. All the air runs through the combustion chamber to provide thrust. A turbofan has a much larger set of blades up front. These push most of the air past the sides of the engine, with only the middle part ... Read More »
Source: http://answers.yahoo.com/question/index?qid=20120503061734AAHAKzC
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Answers to Other Common Questions
A turbo prop has a "jet" engine that drives propellars like on a piston engine plane. Becasue the jet engine spins so fast, there is a gear box that allows the propellar to spin at speeds they normally do. So, the propellar pulls the plan t...
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Source: http://answers.yahoo.com/question/index?qid=20080807110446AA9PLlE
Simple gas turbine system consist of compressor, combustion chamber, and turbine. This system invented by John Barber. Early development of gas turbine, primarily directed toward improvement of compressor efficiency, also the use of turboch...
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Source: http://answers.yahoo.com/question/index?qid=20110122070650AAolwDB
Answer A propeller is completely external and is the main source of propulsion for a airplane with a piston or turbojet engine. A turbofan is more enclosed and provides some propulsion along with also cooling the jet engine that is the main...
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Source: http://wiki.answers.com/Q/What_are_The_differences_between_a_turb...
An engine with a bypass ratio of 2 will pass 2 kg/s of air through the fan for every 1 kg/s through the core. If you know the density and velocity of the two exhausts you could compute the thrust as: T = (rho A V) V where rho = density, A...
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Source: http://en.allexperts.com/q/Aeronautical-Engineering-1809/2009/10/...
A turbojet is one of the oldest kinds of jet engine designs. The air flow enters the jet engine at one end and is compressed while it travels through rows of rotating blades (or stages). It is then ignited in the combustion chamber and as t...
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Source: http://wiki.answers.com/Q/What_is_the_difference_between_a_turbof...
The difference between the low and high bypass turbofans is simply in the amount of air which goes into the engine versus the remainder that goes around (bypasses) the engine. In high bypass engines ( an engine on any large commercial jet) ...
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Source: http://wiki.answers.com/Q/What_is_the_difference_between_high_byp...
what is the difference between a turbofan and a turbojet
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Source: http://wiki.answers.com/Q/What+is+the+difference+between+a+turbof...
