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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
For perfect intercooling in a two stage compressor

p₂/p₁ = p₃/p₂
p₁/p₃ = p₂/p₁
p₁ = p₂ p3
p₁ = p3

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Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Degree of reaction
Pressure coefficient
Slip factor
Work factor

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

10 to 40%
40 to 60%
60 to 70%
70 to 90%

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Compressors, Gas Turbines and Jet Engines
For speed above 3000 km/hour, it is more advantageous to use

Ramjet engine
Propellers
Rockets
Turbojet engine

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

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

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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