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Compressors, Gas Turbines and Jet Engines

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.

One stroke
Four strokes
Three strokes
Two strokes

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

0.83402777777778
0.62569444444444
2.5006944444444
0.41736111111111

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Increase velocity
Convert kinetic energy into pressure energy
Convert pressure energy into kinetic energy
Make the flow streamline

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

None of these
Less than
More than
Equal to

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Compressors, Gas Turbines and Jet Engines
Open cycle gas turbine works on

Ericsson cycle
Brayton or Atkinson cycle
Rankine cycle
Carnot cycle

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Increase
Decrease
None of these
Remain same

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