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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Maximum cycle temperature
All of these
Pressure ratio
Minimum cycle temperature

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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

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

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

kg/m³
m³/min
kg/m²
m³/kg

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isochronically
Isentropically
Adiabatically
Isothermally

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

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

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Compressors, Gas Turbines and Jet Engines
A 3 m³/min compressor means that it

Delivers 3 m³/ min of compressed air
Delivers 3 m³/ min of compressed air at delivery pressure
Compresses 3 m³/min of standard air
Compresses 3 m³/ min of free air

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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