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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

50 bar
20 bar
10 bar
30 bar

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Pressure ratio
Minimum cycle temperature
All of these
Maximum cycle temperature

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

Reheating
All of the listed here
Inter cooling
Adding a regenerator

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Compressors, Gas Turbines and Jet Engines
The work ratio of a gas turbine plant is defined as the ratio of

Net work output and work done by turbine
Net work output and heat supplied
Actual heat drop and isentropic heat drop
Net work output and isentropic heat drop

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Compressors, Gas Turbines and Jet Engines
The fuel consumption in gas turbines is accounted for by

Higher calorific value
Lower heating value
Heating value
Higher heating value

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Compressors, Gas Turbines and Jet Engines
If V, U and Vr represent the absolute velocity of fluid, velocity of blade, and relative velocity of fluid, and suffix ‘I’ and ‘o’ stand for entry and exit conditions, then in a rotary machine whose degree of reaction is unity

Vt > Vo
Vi = Vo
U < Vo
V = Uo

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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