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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is bulky
None of these
It is inefficient
It requires cooling water for its operation

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating compressor, the suction, compression and delivery of air takes place in ________ of the piston.

Four strokes
Two strokes
One stroke
Three strokes

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Radial flow
Axial flow
Centrifugal
None of these

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

1000°C
700°C
200°C
500°C

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