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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

1000°C
700°C
200°C
500°C

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Compressors, Gas Turbines and Jet Engines
The pressure ratio in gas turbines is of the order of

2.5423611111111
0.37569444444444
0.16736111111111
0.084027777777778

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Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

1.00 kg/cm²
1.03 kg/cm²
0.53 kg/cm²
1.06 kg/cm²

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

Polytropic reaction
Pressure coefficient
Work coefficient
Slip factor

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Reduction of speed of incoming air and conversion of part of it into pressure energy
Increasing speed of incoming air
Compression of inlet air
Lost work

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Remain same
Increase
Decrease
Does not change

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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