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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is

6000 KW
15 KW
600 KW
150 KW

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Compressors, Gas Turbines and Jet Engines
A machine used to raise the pressure of air is called

Compressor
I.C engine
Air motor
Gas turbine

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

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

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Compressors, Gas Turbines and Jet Engines
The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)

(v₁² -v₂²)/2g
(v₁² -v₂²)/g
(v₁ - v₂)²/g
(v₁ - v₂)²/2g

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

One air stream
No air stream
Two or more air streams
Solid fuel firing

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