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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The air-fuel ratio in gas turbines is of the order of

7: 1
30: 1
50: 1.
15: 1

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

30 bar
50 bar
10 bar
20 bar

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

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

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

After the inter-cooler
Before first stage suction
Between the after-cooler and receiver
Before the inter-cooler

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

2.2 kg
1.0 kg
1.3 kg
0.5 kg

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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