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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

High altitudes
High speeds
Low altitudes
Low speeds

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

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

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

Centrifugal compressor
All of these
Pumps
Axial compressor

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at

0°C and standard atmospheric conditions
15°C and 1 kg/cm²
20°C and 1 kg/cm² and relative humidity 36%
Atmospheric conditions at any specific location

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Compressors, Gas Turbines and Jet Engines
In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the

Both (A) and (B)
None of these
Efficiency of the engine
Thrust and range of aircraft

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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