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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High altitudes
Low speeds
Low altitudes
High speeds

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Compressors, Gas Turbines and Jet Engines
The thrust of a jet propulsion power unit can be increased by

All of these
Injecting ammonia into the combustion chamber
Injecting water into the compressor
Burning fuel after gas turbine

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Compressors, Gas Turbines and Jet Engines
The efficiency of jet engine is

Same at all altitudes
Higher at high altitudes
Higher at high speed
Lower at low speed

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

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

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance, the work-done on the air during isentropic compression is ________ the heat required to raise the temperature of air from T₁ to T₂ at a constant pressure.

Less than
Greater than
Equal to
None of these

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

70 to 90%
10 to 40%
60 to 70%
40 to 60%

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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