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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The stagnation pressure rise in a centrifugal compressor takes place

In the impeller only
In the diffuser only
In the diffuser and impeller
In the inlet guide vanes only

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

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

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitudes will require ___ power.

Same
None of the listed here
Less
More

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

Carnot cycle
Ericsson cycle
Joule cycle
Rankine cycle

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Compressors, Gas Turbines and Jet Engines
For an irreversible gas turbine cycle, the efficiency and work ratio both depend on

Both pressure ratio and maximum cycle temperature
Pressure ratio alone
Maximum cycle temperature alone
Minimum cycle temperature alone

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

Do not damage turbine blades
Reduces exhaust temperature
Improves thermal efficiency
Increases power output

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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