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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

Same
Low
Low/high depending on make and type
High

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Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

Same
Less
More
May be less or more depending on ambient conditions

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Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

More
Less
Zero
Same

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Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is perpendicular to its axis, then it is a

Axial flow compressor
Reciprocating compressor
Turbo compressor
Centrifugal compressor

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

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Compressors, Gas Turbines and Jet Engines
Mining industry usually employs following motive power

Diesel engine
C. electric motor
Petrol engine
Compressed air

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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