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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

0.41736111111111
0.62569444444444
2.5006944444444
0.83402777777778

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

6 kg/cm²
25 kg/cm²
16 kg/cm²
10 kg/cm²

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

High nickel alloy
High alloy steel
Carbon steel
Stainless steel

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

Increases
None of these
Decreases
Has no effect on

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Atmosphere
Vacuum
Discharge nozzle
Back to the compressor

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.

Higher
Same
None of these
Lower

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