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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Increase of work ratio
Both (A) and (B) above
Decrease of work ratio
Decrease of thermal efficiency

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Compressors, Gas Turbines and Jet Engines
In a compressor, free air delivered is the actual volume delivered at the stated pressure reduced to

N.T.P. conditions
Intake temperature and pressure conditions
20°C and 1 kg/cm²
0°C and 1 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

Less
More
Depends on other factors
Same

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Compressors, Gas Turbines and Jet Engines
Gas turbines for power generation are normally used

In emergency
To supply peak load requirements
To supply base load requirements
To enable start thermal power plant

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

More/less power depending on other factors
More power
Less power
Same power

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler work is known as

Polytropic reaction
Pressure coefficient
Slip factor
Work coefficient

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