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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In gas turbines, high thermal efficiency is obtained in

Open cycle
Closed cycle & Open cycle
Closed/open depending on other considerations
Closed cycle

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

None of the listed here
Free air delivery
Swept volume
Compressor capacity

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

All of these
Higher volumetric efficiency
Decreased discharge temperature
Lower power consumption per unit of air delivered

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Isentropic compression
Adiabatic compression
Isothermal compression
Polytropic compression

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

Cooling chamber
Heating chamber
Compressor
All of these

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Compressors, Gas Turbines and Jet Engines
Which of the following plants is smallest and lightest for generating a given amount of power?

Solar plant
Gas turbine plant
Diesel engine
Petrol engine

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