Turbofans and turboprops Flashcards

1
Q

What is central to the design of the turbofan?

A

the by-pass ratio

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2
Q

What is the by-pass ratio?

A

the ratio between the mass flow rate of air drawn in by the fan but bypassing the engine core to the mass flow rate passing through the engine core

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3
Q

What does a high bypass ratio give?

A

a lower exhaust speed

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4
Q

What does a lower bypass ratio give?

A

a higher exhaust speed

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5
Q

What is a higher exhaust speed needed to sustain?

A

supersonic airspeeds

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6
Q

What is a turboprop?

A

a direct extension of the piston-engine propeller system, where the piston engine is replaced by a gas turbine

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7
Q

What is the purpose of air intake?

A

*increases pressure by the ram-effect
*ensures uniform flow to the compressor under diverse aircraft incidences

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8
Q

What does air intake not involve?

A

heat or work exchange with its surroundings

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9
Q

What happens at the air intake?

A

there is an interchange between kinetic energy and the enthalpy of the gas
this means the flow slows down and the pressure and temperature go up

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10
Q

What is true about compression in subsonic regimes?

A

compression is realised smoothly

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11
Q

What happens if area increase is abrupt in subsonic regimes?

A

risk of flow separation

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12
Q

What does the intake of air affect?

A

the engine performance and the flow around the engine

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13
Q

What problems may arise with military aircrafts?

A

problems with boundary layer ingestion

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14
Q

What are the main difficulties at supersonic regimes?

A

the main difficulties arise because of a smooth compression from supersonic to subsonic, which is practically impossible to achieve

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15
Q

What does compression in supersonic regimes almost always involve?

A

shock waves

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