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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

Pressure coefficient
Euler
Isentropic efficiency
Compressor efficiency

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Compressors, Gas Turbines and Jet Engines
Open cycle gas turbine works on

Ericsson cycle
Rankine cycle
Brayton or Atkinson cycle
Carnot cycle

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To increase the efficiency
To save fuel
To reduce the exit temperature
To increase the output

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Compressors, Gas Turbines and Jet Engines
In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the

None of these
Efficiency of the engine
Thrust and range of aircraft
Both (A) and (B)

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

Multistage compression without intercooling
Single stage compression
Multistage compression with intercooling
None of these

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

All of these
Compressor
Cooling chamber
Heating chamber

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