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Compressors, Gas Turbines and Jet Engines

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

Brayton or Atkinson cycle
Ericsson cycle
Carnot cycle
Rankine cycle

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Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Isothermal compression
Ideal compression
Isentropic compression
Adiabatic compression

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Compressors, Gas Turbines and Jet Engines
The efficiency of roots blower ________ with the increase in pressure ratio.

None of these
Decreases
Does not change
Increases

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Decrease
Remain same
None of these
Increase

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is bulky
It requires cooling water for its operation
None of these
It is inefficient

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered in a medium capacity air compressor per unit time is

None of these
Above 5 m³/s
0.1 to 1.2 m³/s
0.15 to 5 m³/s

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