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Compressors, Gas Turbines and Jet Engines

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 two phases
In three phases

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Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Reduce volume of air
Cause moisture and oil vapour to drop out
Remove impurities from air
Cool the air

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Compressors, Gas Turbines and Jet Engines
The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

Less than
More than
None of these
Equal to

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

High alloy steel
Carbon steel
Stainless steel
High nickel alloy

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Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Compression work/motor input
Isothermal H.P/indicated H.R
Total output/air input
Isothermal H.P./shaft H.R

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Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Pressures across the turbine
Inlet pressure to exhaust pressure
Compressor pressure ratio
Highest pressure to exhaust pressure

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