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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

Same
More
Less
Zero

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Centrifugal pump
Turbine
Reciprocating pump
Sliding vane compressor

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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
None of these
Equal to

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Compressors, Gas Turbines and Jet Engines
The work ratio of a gas turbine plant is defined as the ratio of

Net work output and heat supplied
Actual heat drop and isentropic heat drop
Net work output and work done by turbine
Net work output and isentropic heat drop

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Compressors, Gas Turbines and Jet Engines
Adiabatic compression is one in which

Temperature rise follows a linear relationship
No heat leaves or enters the compressor cylinder during compression
Temperature during compression remains constant
Work done is maximum

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Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating air compressor, without clearance, the compression of air may be

Isothermal
Polytropic
Any one of these
Isentropic

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