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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Air-fuel ratio in a jet engine will be of the order of

0.83402777777778
0.41736111111111
2.5006944444444
0.62569444444444

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Cools the delivered air
Results in saving of power in compressing a given volume to given pressure
Is the standard practice for big compressors
Enables compression in two stages

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In a single phase
In two phases
In the form of air and water mixture

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered in a medium capacity air compressor per unit time is

Above 5 m³/s
0.1 to 1.2 m³/s
None of these
0.15 to 5 m³/s

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Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Ideal compression
Isentropic compression
Isothermal compression
Adiabatic compression

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

High h.p. and low weight
Low weight and small frontal area
Small frontal area and high h.p.
High speed and high h.p.

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