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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is inefficient
None of these
It is bulky
It requires cooling water for its operation

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

Equal to
More than
Less than
None of these

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Compressors, Gas Turbines and Jet Engines
The performance of air compressor at high altitudes will be ________ as compared to that at sea level.

None of these
Lower
Same
Higher

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Compressors, Gas Turbines and Jet Engines
A jet engine works on the principle of conservation of

Mass
Linear momentum
Energy
Flow

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Compressors, Gas Turbines and Jet Engines
Free air is the air at

Atmospheric conditions at any specific location
0°C and standard atmospheric conditions
20°C and 1 kg/cm² and relative humidity of 36%
15°C and 1 kg/cm²

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Decreases the thermal efficiency
Increases the turbine work
Increases the compressor work
Increases the thermal efficiency

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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