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Compressors, Gas Turbines and Jet Engines

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

Euler
Compressor efficiency
Isentropic efficiency
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

In never used
Provides lesser flexibility
Is used when gas is to be burnt
Provides greater flexibility

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

2.5423611111111
0.16736111111111
0.37569444444444
0.084027777777778

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Control temperature
Control fire hazards
Control output of turbine
Increase efficiency

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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