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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Isothermal H.P/indicated H.R
Isothermal H.P./shaft H.R
Compression work/motor input
Total output/air input

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Atmosphere
Vacuum
Discharge nozzle
Back to the compressor

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Euler
Isentropic efficiency
Pressure coefficient
Compressor efficiency

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

Between the after-cooler and receiver
Before first stage suction
After the inter-cooler
Before the inter-cooler

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Compressors, Gas Turbines and Jet Engines
A rocket works with maximum overall efficiency when air craft velocity is equal to the

Average of the jet velocity
Half the jet velocity
Jet velocity
Twice the jet velocity

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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

Slip factor
Pressure ratio
Degree of reaction
Pressure coefficient

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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