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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

Critical pressure
None of the listed here
Back pressure
Discharge pressure

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

0.5 kg
2.2 kg
1.0 kg
1.3 kg

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

between ~ to i of the blade height
at the tip
at the base
in the center

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

They can generate very high thrust
These engines can work on several fuels
They have high propulsion efficiency
They are not air breathing engines

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Compressors, Gas Turbines and Jet Engines
For slow speed large capacity compressor, following type of valve will be best suited

Mechanical valve of the Corliss, sleeve, rotary or semi rotary type
Poppet valve
Any of the above
Disc or feather type

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In the form of air and water mixture
In two phases
In a single phase

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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