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

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Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Highest
Atmospheric
Anything
Lowest

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Axial flow compressors
Pumps
All of these
Radial flow compressors

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Rankine cycle
Carnot cycle
Ericsson cycle
Brayton or Atkinson cycle

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the compressed air main line should

Be laid exactly horizontally
Drop gradually towards the point of use
Rise gradually towards the point of use
Be laid vertically

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

Work coefficient
Slip factor
Pressure coefficient
Polytropic reaction

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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