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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Nitrogen
Ammonia and water vapour
Carbon dioxide
Hydrogen

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Ramjet engine
Gas turbine engine equipped with a propulsive nozzle and diffuse
A propeller system
Chemical rocket engine

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

40 to 60%
60 to 70%
70 to 90%
10 to 40%

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Compressors, Gas Turbines and Jet Engines
The minimum work required for a three stage reciprocating air compressor is ___ the work required for each stage.

Double
Three times
Six times
Equal to

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Compressors, Gas Turbines and Jet Engines
The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)

r ɣ-1
1 - (1/r) ɣ-1/ɣ
1 - (1/r) ɣ/ɣ-1
1 - r ɣ-1

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

Axial flow type
None of these
Radial flow type
Centrifugal type

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