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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)

W₂/(W₁ + W₂)
W₁/(W₁ + W₂)
(W₁ + W₂)/W₂
(W₁ + W₂)/W₁

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Compressors, Gas Turbines and Jet Engines
Rotary compressors are suitable for

Large discharge at high pressure
Low discharge at low pressure
Large discharge at low pressure
Low discharge at high pressure

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Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Inlet pressure to exhaust pressure
Pressures across the turbine
Compressor pressure ratio
Highest pressure to exhaust pressure

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

50 bar
30 bar
20 bar
10 bar

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Compressors, Gas Turbines and Jet Engines
The efficiency and work ratio of a gas turbine plant can be increased by

Injecting water in/around combustion chamber
All of these
Reheating the air after partial expansion in the turbine
Adding heat exchanger

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller in front
Propeller on the top
Propeller at back
No propeller

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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