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Compressors, Gas Turbines and Jet Engines

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

Carbon steel
High nickel alloy
High alloy steel
Stainless steel

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

700°C
200°C
500°C
1000°C

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of air compressors is of the order of

60 - 70%
70 - 90%
40 - 50%
20 - 30%

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Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Reduce volume
Decrease the delivery temperature for ease in handling
Cause moisture and oil vapour to drop out
Cool the air

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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
16 kg/cm²
10 kg/cm²
25 kg/cm²

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Compressors, Gas Turbines and Jet Engines
In a closed cycle gas turbine, the air is compressed

Isothermally
None of these
Polytropically
Isentropically

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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