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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Thrust power and propulsive power
Propulsive power and fuel input
Engine output and propulsive power
Thrust power and fuel energy

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Compressors, Gas Turbines and Jet Engines
In a compressor, free air delivered is the actual volume delivered at the stated pressure reduced to

Intake temperature and pressure conditions
20°C and 1 kg/cm²
0°C and 1 kg/cm²
N.T.P. conditions

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

at the tip
in the center
at the base
between ~ to i of the blade height

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Increase
Other factors control it
Remain unaffected
Decrease

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor

Decreases with decrease in compression ratio
Increases with decrease in compression ratio
Decreases with increase in compression ratio
Increases with increase in compression ratio

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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