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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor without clearance volume, the work-done is maximum during

None of these
Polytropic compression
Isothermal compression
Isentropic compression

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Thrust power and fuel energy
Propulsive power and fuel input
Engine output and propulsive power
Thrust power and propulsive power

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

6 kg/cm²
10 kg/cm²
25 kg/cm²
16 kg/cm²

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Electric motor
Engine
None of these
Either (A) or (B)

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

Does not change
None of these
Decreases
Increases

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

Increased inclination of chord with air steam
No flow of air
Reducing mass flow rate with increase in pressure ratio
Fixed mass flow rate regardless of pressure ratio

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