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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases
Increases/decreases depending on compressor capacity
Decreases
Remains same

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High speeds
Low speeds
High altitudes
Low altitudes

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Compressors, Gas Turbines and Jet Engines
A closed gas turbine in which fuel is burnt directly in the air is not possible because of

High specific volume
High friction losses
Paucity of O2
Increasing gas temperature

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

1.0%
5%
0.1%
0.5%

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

1000°C
1500°C
700°C
2000°C

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

After receiver
Between after-cooler and air receiver
Before inter-cooler
After inter-cooler

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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