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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

Low altitudes
Low speeds
High speeds
High altitudes

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is inefficient
It is bulky
None of these
It requires cooling water for its operation

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Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Collect more air
Convert kinetic energy of air into pressure energy
Provide robust structure
Beautify the shape

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Compressors, Gas Turbines and Jet Engines
The compressed air may be used

In gas turbine plants
In starting and supercharging of I.C. engines
For operating pneumatic drills
All of the listed here

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Compressors, Gas Turbines and Jet Engines
For maximum work, the reheating should be done to an intermediate pressure of (Where p₁ = Maximum pressure, and p₂ = Minimum pressure)

p₁/p₂
(p₁ - p₂)/2
(p₁ + p₂)/2
p₁ p₂

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Compressors, Gas Turbines and Jet Engines
During base load operation, the best method of controlling compressor is

Start-stop motor
Constant speed unloader
Variable speed
Relief valve

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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