What is the mass flow rate of a jet engine?

What is the mass flow rate of a jet engine?

According to The GE90 – An Introduction, the GE90 has a mass flow rate of 1,350 kg/s at take-off and 576 kg/s at cruise (at 10.668 km = FL350). The CF6 has a mass flow rate of 591 kg/s at take-off.

What’s the difference between turbojet and turbofan?

Unlike a turbojet that sucks in all the air inside the engine, a turbofan engine sports a large fan at the front which sucks in most of the airflow around the outside of the engine. This makes the engine quieter and more thrust at low speeds. A majority of all the airliners are powered by this engine.

How do you calculate mass flow rate?

Mass flow rate can be calculated by multiplying the volume flow rate by the mass density of the fluid, ρ. The volume flow rate is calculated by multiplying the flow velocity of the mass elements, v, by the cross-sectional vector area, A.

What are the mass flow rate and exhaust velocity for a CF6 or GE90?

What are the mass flow rate and exhaust velocity for a CF6 or GE90 turbofan? For a typical turbofan jet engine (two examples given in the title), what is the exhaust velocity and mass flow rate of air at sea level and cruising altitude (~ FL350)?

What is the bypass ratio of a turbofan engine?

The bypass ratio (BPR) of a turbofan engine is the ratio between the mass flow rate of the bypass stream to the mass flow rate entering the core. A 10:1 bypass ratio, for example, means that 10 kg of air passes through the bypass duct for every 1 kg of air passing through the core.

For a typical turbofan jet engine (two examples given in the title), what is the exhaust velocity and mass flow rate of air at sea level and cruising altitude (~ FL350)? Also, does the specific impulse vary at different altitudes, since the density of air decreases with increases in altitude?

Why does a turbofan generate more thrust than a fan?

We can combine the terms multiplying V0 and use the definition of the bypass ratio bpr to obtain the final thrust equation: Because the fuel flow rate for the core is changed only a small amount by the addition of the fan, a turbofan generates more thrust for nearly the same amount of fuel used by the core.