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COMPRESSORS, GAS TURBINES AND JET ENGINES

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

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

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In two phases
In three phases
In a single phase
In the form of air and water mixture

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Compressors, Gas Turbines and Jet Engines
An air receiver is to be placed outside. Should it be placed in

Rain
Shade
Enclosed room
Sun

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Compressors, Gas Turbines and Jet Engines
In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the

Both (A) and (B)
Efficiency of the engine
Thrust and range of aircraft
None of these

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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)

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

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