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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Ericsson cycle
Carnot cycle
Brayton or Atkinson cycle
Rankine cycle

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Compressors, Gas Turbines and Jet Engines
A turboprop is preferred to turbojet because

It has high power for take off
It can fly at supersonic speeds
It has high propulsive efficiency at high speeds
It can fly at high elevations

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Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating compressor, the suction, compression and delivery of air takes place in ________ of the piston.

Three strokes
Two strokes
One stroke
Four strokes

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Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Pressure ratio
Pressure coefficient
Slip factor
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)

1 - (1/r) ɣ/ɣ-1
1 - r ɣ-1
r ɣ-1
1 - (1/r) ɣ-1/ɣ

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Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Cool the air
Reduce volume
Decrease the delivery temperature for ease in handling
Cause moisture and oil vapour to drop out

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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