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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

2 kg/cm²
14.7 kg/cm²
6 kg/cm²
10 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Less
More
Same
Zero

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

Opposite to the direction of motion of blades
In the direction of motion of blades
Equal to zero
Depending on the velocity

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Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.2
0.3
0.4
0.5

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Compressors, Gas Turbines and Jet Engines
For minimum work required to compress and deliver a quantity of air by multistage compression

The work-done in each stage should be same
The compression ratio in each stage should be same
All of the listed here
The intercooling should be perfect

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Decreased discharge temperature
Lower power consumption per unit of air delivered
Higher volumetric efficiency
All of these

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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