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Compressors, Gas Turbines and Jet Engines

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
More
Less
May be less or more depending on ambient conditions

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Compressors, Gas Turbines and Jet Engines
A jet engine has

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

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

700°C
200°C
500°C
1000°C

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Does not require oxygen
Uses compressed atmospheric air
Carries its own oxygen
Uses surrounding air

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase speed
Reduce turbine size
Increase temperature
Increase power output

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isochoric
Isentropic
Isothermal
Adiabatic

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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