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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

None of the listed here
Isentropic compression
Isothermal compression
Polytropic compression

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

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

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

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

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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
Lost work
Compression of inlet air
Increasing speed of incoming air

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Carries its own oxygen
Uses surrounding air
Uses compressed atmospheric air
Does not require oxygen

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Compressors, Gas Turbines and Jet Engines
When the temperature of air leaving the inter-cooler, in a two stage compression with inter-cooler, is ________ the original atmospheric air temperature, then the intercooling is known as perfect or complete intercooling.

More than
Less than
Equal to
None of these

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